sabeing evaluated using eddy current inspection techniques. the unique capabilities of e-probes and...

70
NASA Technical Memorandum NASATM-103567 FY 1991 SCIENTIFIC AND TECHNICAL REPORTS, ARTICLES, PAPERS, AND PRESENTATIONS Compiled by Joyce E. Turner Management Operations Office October 1991 ( (NASA-TM-103567) FY 1991 SCIENTIFIC AND TECHNICAL REPORTS, ARTICLES, PAPERS, AND PRESENTATIONS i!(NASA) 69 p CSCL 05B I G3/82 N92-17586 Uncl as 0070340 fW\SA National Aeronautics and Space Administration George C. Marshall Space Flight Center MSFC - Form 3190 (Rev. May 1983) https://ntrs.nasa.gov/search.jsp?R=19920008367 2020-03-23T15:13:22+00:00Z

Upload: others

Post on 18-Mar-2020

8 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASATechnicalMemorandum

NASATM-103567

FY 1991 SCIENTIFIC AND TECHNICAL REPORTS,ARTICLES, PAPERS, AND PRESENTATIONS

Compiled by Joyce E. TurnerManagement Operations Office

October 1991

( (NASA-TM-103567) FY 1991 SCIENTIFIC ANDTECHNICAL REPORTS, ARTICLES, PAPERS, ANDPRESENTATIONS i!(NASA) 69 p CSCL 05B

IG3/82

N92-17586

Uncl as0070340

fW\SANational Aeronautics andSpace Administration

George C. Marshall Space Flight Center

MSFC - Form 3190 (Rev. May 1983)

https://ntrs.nasa.gov/search.jsp?R=19920008367 2020-03-23T15:13:22+00:00Z

Page 2: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

1-0

s=

oi-i«O"i*"':

;rij!>•Xjx

Ojx.Eli

-0oj£PJ:"!

cTj• —1pr-i

rnCOLUUJ

•I ;.

~Z?li.

itCCUJcn— i

LUCDj;

21r— i

•g7

LULUjV[

oCO

...taOj

•r-i

iTT

h-!

<LCO3:

OS

3=f—ii_;V

CU03

>CCOCDLuI —<ECJ

inOJ[X

T-i

LUIT}

<rLi-

eu•r-i

i>

\ LUCXI H3\ cnCO COO1 r— i

>-<T

_i *a. *cn -sOr-i — i

Q 0-'~J>-

— -t

"

Oo-

H-2LUSDO~i

:— 'Q

QLUr-i

ij_i-i

COCO<d_fCJz— r

COLUrn<fiX

CD•Jj

Oox.O'-i

xG*1

03

~TCDcn\_.:O1

'-i==in•>-i

=

•r-i

-GrS

-ij!5

iuOLiT3ac.

if:0!

.— i

!J• i-f•pi_

03

r.

U'i-P•

O

Q-il!<_

r-i

03

U.r-i

Cx:uCU-PTjt—

ty

U• r-i

^-.i-i

-P

C i/!in c•l-i O

U -^in -P

f5i> -p

CO Ci> CU,-i ai

CU;;- L.

LL. D.

— iH-:

b

a

Q.i=

OuX<L

c:

i—«

0-

«LU

LUQ;j-OT~-j

'•

~f'

Uj

E2XirX

-ri —^~i

<I

-P

XI

•ri

r-i

LL

QjUrSa

cn1— tr-i

nsx;iTit_03i.

»CO•ri

-P

03

i_

-P

Li• r<

C•rH

£

T3<E

CUu•13a.

CO1-1

T3 Oi— = ^T* _1

<I LLs/: s:U "• X

•=-i as <r-P r-i O

3 r-i <T

03 -ri

z > uo ui x cnu .P ujCU C CO :—<I -t M l <L

"f | — U—

"-* Z COm -C !- " Qu 5i =-i Lu.ri ^ .ri i—

•P C 03 r-i

0; di > ~

Z O <I t3

0- 35 «o; a. oO <T r-i

cj cn u

X:'i-i'-?•'f j

""•

<f

-^

i_Jixi—cn.'T

*X

COLUCJr?LUi—irjb'J

LUCJ<I0.cnD2LU<L

*^CDZr-i

ii;LULUZt— t

rn__.

LU

LUfj<T

£LDTOLuLU<rx O'jcn LUCJ i-ir-i -L.

V- Q-~i <E<r ="•? CD0 00; >-<UJ -1<I «dC i—i

X ffi

cni~3

c^z

CD!— i

cnLUD

U_<L

CJUJai _03

•x_

0"Ja:LU

••OCu_

X03LU

d5— i

XLU

T"

CJz_-l

_J

x1-'•£.Ozo;V

1 —CO

x~?CD-_ .COLU

j—LL•CE

O •-Ct! u. . t !—

'I -P

^JX. <T

O'J "i <ni — £ CC$

Z <E

x:

ilji_

•n!> £Cti ai0 ;_•*"* O

>• £_Q ~

T3OJ-P

4imCUi_Q.

Ul;_'dfLJ_

Q.

uJ^

u:CULIciiuli-eu;_

U

;.—

CL

!_

ij^

O-i-i

r-i_Q

.r-i

J-i

ij_

O

e—\• r-lT3

isaoLJ

<r

>a

03

'-1

> &LL £

cn «••C if!

!_ i_

J OT3 Q.

Fj^_

O r-i

•P iTj

U Usti -rii_ ;—

-P jC U0 Q;U -P

TJ <rf" ''n03 'C11"

Z

Qj r-i

C ffiC Su i-ai oi i __ffla asTJ

•~- 3CJ r-i

U. Ucn c2: -ri•

Ui

S 5" IlL

a exCJ

SJ: "i .—

r~ i —QI

•>-i 3-« "OU. CU

CU -rtu >fu O0. !_

cn a

>•X3

ui &c >O ;u

• r-i _C

-P

Oi 03-^ T3•r; i-

Q) hjLH UCU 0i- j=D. Qi

cIDc -aOi C

05

in mr-i -p

S! L.C 0t- Q.3 OiO !_•*^

c—i

-« 0503 uU -rt

•ri C

C XTx: uu cuOJ '-P

-•i.c cn•" <L

^LT301 rH

r- asyi e

• r-i !_

r-i ij

X! H-3a. QJ

1-CU 1-

5 =3 r-i

0!r" r~"0 £•ri O

s: uiS i_

s/i a:_

iu oQ. j _

03 CO

DU:r-i

03

Oii_

ili

ui-Pr~5g3U0

T3

CUUiCUx:-P

?'..-iC.ri

03-PX3ol__

o4-

UlCUui

3JJ

cn»

"acu-gr-iuc.ri

Ul 3

-^ Tiu o.!03 "ni- 3•P rH

Ui U

X! |I03 -ri

ZLU

Page 3: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

REPORT DOCUMENTATION PAGEForm Approved

OMB No. 0704-0188

Public reporting burden for this collection of information is estimated to average t hour per response, including the time for reviewing instructions, searching existing data sources,gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of thiscollection of information, including suggestions for reducing this burden, to Washington Headquarters Services. Directorate for Information Operations and Reports. 1215 JeffersonDavis Highway. Suite 1204. Arlington. VA 22202-4302, and to the Office of Management and Budget. Paperwork Reduction Project (0704-0188). Washington. DC 20503.

1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE

October 19913. REPORT TYPE AND DATES COVERED

Technical Memorandum4. TITLE AND SUBTITLE

FY 1991 Scientific and Technical Reports, Articles, Papers, andPresentations

6. AUTHOR(S)

Compiled by Joyce E. Turner

5. FUNDING NUMBERS

7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)

George C. Marshall Space Flight CenterMarshall Space Flight Center, Alabama 35812

8. PERFORMING ORGANIZATIONREPORT NUMBER

9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES)

National Aeronautics and Space AdministrationWashington, DC 20546

10. SPONSORING/MONITORINGAGENCY REPORT NUMBER

NASA TM-103567

11. SUPPLEMENTARY NOTES

Prepared by Management Operations Office, Administrative Operations Office

12a. DISTRIBUTION/AVAILABILITY STATEMENT

Unclassified - Unlimited

12b. DISTRIBUTION CODE

13. ABSTRACT (Maximum 200 words)

This document presents formal NASA technical reports, papers published in technicaljournals, and presentations by MSFC personnel in FY91. It also includes papers of MSFCcontractors.

After being announced in STAR, all of the NASA series reports may be obtained from theNational Technical Information Service, 5285 Port Royal Road, Springfield, VA 22161.

The information in this report may be of value to the scientific and engineering communityin determining what information has been published and what is available.

14. SUBJECT TERMS 15. NUMBER OF PAGES

6916. PRICE CODE

NTIS17. SECURITY CLASSIFICATION

OF REPORTUnclassified

18. SECURITY CLASSIFICATIONOF THIS PAGE

Unclassified

19. SECURITY CLASSIFICATIONOF ABSTRACT

Unclassified

20. LIMITATION OF ABSTRACT

UnlimitedNSN 7540-01-280-5500 Standard Form 298 (Rev. 2-89)

Prescribed by ANSI Std. Z39-18298-102

Page 4: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

FOREWORD

In accordance with the NASA Space Act of 1958, the MSFC has provided for thewidest practicable and appropriate dissemination of information concerning its activities andthe results thereof.

Since July 1, 1960, when the George C. Marshall Space Flight Center was organized,the reporting of scientific and engineering information has been considered a primeresponsibility of the Center. Our credo has been that "research and development work isvaluable, but only if its results can be communicated and made understandable to others."

The N number shown for the reports listed is assigned by the Center for AeroSpaceInformation (CASI), Baltimore, Maryland, indicating that the material is unclassified andunlimited and is available for public use. These publications can be purchased from theNational Technical Information Service, 5285 Port Royal Road, Springfield, Virginia 22161.The N number should be cited when ordering.

PRECEDING PAGE BLANK NOT F1LWTED

Page 5: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

GEORGE C. MARSHALL SPACE FLIGHT CENTERMarshall Space Flight Center, Alabama

FY 1991 SCIENTIFIC AND TECHNICAL REPORTS,ARTICLES, PAPERS, AND PRESENTATIONS

TABLE OF CONTENTS

Page

NASA TECHNICAL MEMORANDA 1

NASA TECHNICAL PAPERS 12

MSFC CONFERENCE PUBLICATIONS 15

NASA REFERENCE PUBLICATIONS 16

NASA CONTRACTOR REPORTS 17

MSFC PAPERS CLEARED FOR PRESENTATION 28

IV

Page 6: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

TM-103514 October 1990Eddy Current Inspection of Graphite FiberComponents. Dr. G.L. Workman and C.C.Bryson. Materials and Processes Labora-tory. N91-10294

The recognition of defects in materialsproperties still presents a number of problemsfor nondestructive testing in aerospace systems.This project attempts to utilize current capabili-ties in eddy current instrumentation, artificialintelligence, and robotics in order to provideinsight into defining geometrical aspects of flawsin composite materials which are capable ofbeing evaluated using eddy current inspectiontechniques. The unique capabilities of E-probesand horseshoe probes for inspecting probes forinspecting graphite fiber materials have beenevaluated and appear to hold great promise oncethe technology development matures.

This preliminary phase report describes theinitial results of modeling eddy current inter-actions with certain flaws in graphite fibersamples.

TM-103515 October 1990Test and Model Correlation of theAtmospheric Emission Photometric ImagerFiberglass Pedestal. H.M. Lee III and L.A.Barker. Structures and Dynamics Labora-tory. N91-13766

This report presents the correlation of thestatic loads testing and finite element modelingfor the fiberglass pedestal used on theAtmospheric Emission Photometric Imaging(AEPI) experiment. This payload is to belaunched in the space shuttle as part of theATLAS-1 experiment. Strain gauge data fromrosettes around the highly loaded base arecompared to the same load case run for theSpacelab 1 testing done in 1981. Correlation ofthe model and test data was accomplishedthrough comparison of the composite stressinvariant utilizing the expected flight loads forthe ATLAS-1 mission. Where appropriate, theTsai-Wu failure criteria was utilized in thedevelopment of the key margins of safety.Margins of safety are all positive for the pedestaland are reported,

TM-103516 September 1990Coaligned Observations of Solar MagneticFields at Different Heights—MSFC Center

Director's Discretionary Fund Final Report(Project Number 88-10). MJ. Hagyard, E.A.West, G.A. Gary, and J.E. Smith, SpaceScience Laboratory. N91-10832

This document constitutes the final report forMSFC Center Director's Discretionary FundProject Number 88-10. The objective of thisprogram was to develop the capability for obtain-ing cotemporal and coaligned observations of thestructure and evolution of the Sun's magneticfield at two different heights in the solaratmosphere: the photosphere, which is thelowest region observable with optical tele-scopes, and the chromosphere, which lies justabove the photosphere and is a region where themagnetic field dominates the gas motions so thata well-ordered structure governed by the field isobserved. By obtaining this three-dimensionalpicture of the solar magnetic field, we candevelop a better understanding of the magneticforces that produce and control the dynamic,high-energy phenomena occurring in the solaratmosphere that can affect the entire helio-sphere, including our own terrestrial environ-ment.

TM-103517 October 1990An Improved Exploratory Search Techniquefor Pure Integer Linear ProgrammingProblems. F.R. Fogle. Systems Analysis andIntegration Laboratory. N91-13910

This report documents the development of aheuristic procedure for the solution of pureinteger linear programming problems. The proce-dure draws its methodology from the ideas of theHooke and Jeeves type I and type II exploratorysearches, greedy procedures, and neighborhoodsearches. It utilizes an efficient rounding pro-cedure to obtain its first feasible integer pointfrom the optimal continuous solution obtained viathe simplex method.

Since this procedure is based entirely onsimple addition or subtraction of one to eachvariable of a point in n-space and the subsequentcomparison of candidate solutions to a given setof constraints, it facilitates significant complexityimprovements over existing techniques. It alsoobtains the same optimal solution found by thebranch-and-bound technique in 44 out of 45small to moderate size test problems. Twoexample problems are worked in detail toshow the inner workings of the procedure.

Page 7: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

Furthermore, using an established weightedscheme for comparing computational effortinvolved in an algorithm, a comparison of thisalgorithm is made to the more established andrigorous branch-and-bound method. A computerimplementation of the procedure, in PC-compatible Pascal, is also presented anddiscussed. This procedure for finding optimalsolutions to integer-type problems may beapplied to various systems engineeringsituations in the conceptual, preliminary, anddetail design phases of the system developmentcycle.

TM-103518 November 1990Dendritic Morphology and Microsegregationin Directionally Solidified Superalloy, PWA-1480, Single Crystal: Effect of Gravity-Center Director's Discretionary Fund Report.S.N. Tewari, M.V. Kumar, I.E. Lee, and P.A.Curreri. Materials and Processes Labora-tory. N91-15391

Primary dendrite spacings, secondary den-drite spacings, and microsegregation have beenexamined in PWA-1480 single crystal speci-mens which were directionally solidified duringparabolic maneuvers on the KC-135 aircraft.Experimentally observed growth rate andthermal gradient dependence of primary dendritespacings are in good agreement with predictionsfrom dendrite growth models for binary alloys.Secondary dendrite coarsening kinetics show areasonable fit with the predictions from ananalytical model proposed by Kirkwood for abinary alloy. The partition coefficients oftantalum, titanium, and aluminum are observedto be less than unity; while that for tungsten andcobalt are greater than unity. This is qualitativelysimilar to their nickel base binaries. Micro-segregation profiles experimentally observed forPWA-1480 superalloy show a good fit withBower, Brody, and Flemings models developedfor binary alloys. Transitions in gravity levels donot appear to affect primary dendrite spacings. Atrend of decreased secondary arm spacings withtransition from high gravity to the low gravityperiod was observed at a growth speed of 0.023cm s~l. However, definite conclusions can onlybe drawn by experiments at lower growthspeeds which make it possible to examine theside-branch coarsening kinetics over a longerduration. Such experiments, not possible due to

the insufficient low-gravity time of the KC-135,may be carried out in the low-gravityenvironment of space.

TM-103519 October 1990Engineering Design Based on Risk—AnAlternate Criterion to the Engineering SafetyFactor. D.R. Moore. Materials and Pro-cesses Laboratory. X91 -10073

The design of engineering structures can bebased on risk when enough information about thestructure is available. This report comparesdesigning by risk to the more commonly usedapproach of designing by an engineering factor ofsafety. The safety factor concept of providingstructural assurance is challenged within thisreport. New methods are developed to assist indetermining structural risk in an engineeringdesign when the design is based on the inter-ference of two normally distributed engineeringphenomena. The risk factor (Rp) approach isoffered as an alternate method of establishingengineering design criteria. The engineering riskequation is developed which allows a simpledetermination of risk when coefficients of varia-tion are known. Several curves were developedthat relate Rp to coefficients of variation forvarious reliabilities. The author concluded thatdesigns and redesigns should be based on riskwhenever possible.

TM-103520 October 1990FY 1990 Scientific and Technical Reports,Articles, Papers, and Presentations.Compiled by Joyce E. Turner. ManagementOperations Office. N91-15926

This document presents formal NASA tech-nical reports, papers published in technicaljournals, and presentations by MSFC personnelin FY90. It also includes papers of MSFC con-tractors.

After being announced in STAR, all of theNASA series reports may be obtained from theNational Technical Information Service, 5285Port Royal Road, Springfield, VA 22161.

Hie information in this report may be of valueto the scientific and engineering community indetermining what information, has been publishedand what is available.

Page 8: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

TM-103521 November 1990Predicting Thunderstorm Evolution UsingGround-Based Lightning Detection Net-works. Steven J. Goodman. Space ScienceLaboratory. N91-15660

Lightning measurements acquired principallyby a ground-based network of magnetic directionfinders are used to diagnose and predict theexistence, temporal evolution, and decay ofthunderstorms over a wide range of space andtime scales extending over four orders ofmagnitude. The nonlinear growth and decay ofthunderstorms and their accompanying cloud-to-ground lightning activity is described by the threeparameter logistic growth model. The growthrate is shown to be a function of the storm sizeand duration, and the limiting value of the totallightning activity is related to the availableenergy in the environment. A new technique isdescribed for removing systematic bearing errorsfrom direction finder data where radar echoes areused to constrain site error correction andoptimization (best point estimate) algorithms. Anearest neighbor pattern recognition algorithm isemployed to cluster the discrete lightning dis-charges into storm cells, and the advantages andlimitations of different clustering strategies forstorm identification and tracking are examined.

TM103522 November 1990The Rotating Spectrometer: New Biotech-nology for Cell Separations. David A. Noeverand Helen C. Matsos. Space Science Lab-oratory. N91-15673

An instrument for biochemical studies, calledthe rotating spectrometer, separates previouslyinseparable cell cultures. The rotating spec-trometer is intended for use in pharmacologicalstudies which require fractional splitting ofheterogeneous cell cultures based on cell mor-phology and swimming behavior. As a method toseparate and concentrate cells in free solution,the rotating method requires active organismparticipation and can effectively split the largeclass of organisms known to form spontaneouspatterns. Examples include the biochemical"star," an organism called Tetrahymenapyriformis. Following focusing in a rotated frame,the separation is accomplished using differentradial dependencies of concentrated algal andprotozoan species. The focusing itself appears asconcentric rings and arises from the coupling

between swimming direction and Coriolis forces.A dense cut is taken at varying radii andextraction is replenished at an inlet. Unlikestandard separation and concentrating tech-niques such as filtration or centrifugation, theinstrument is able to separate motile fromimmotile fractions. For a single pass, typical splitefficiencies can reach 200 to 300 percent com-pared to the inlet concentration.

TM-103523 November 1990A Biosensor for Cadmium Based on Biocon-vective Patterns. David A. Noever andHelen C. Matsos. Space Science Laboratory.

N91-15674r

An in vitro method for monitoring cadmium,one of the most lethal bivalent heavy metals, candetect biologically active levels. The effects ofcadmium tend to concentrate in protozoa farabove natural levels and therein begin trans-ferring through freshwater food chains to animalsand humans. In a small sample volume (~5 ml)the method uses the toxic response to the proto-zoa, Tetrahymena pyriformis, to cadmium. Theassay relies on macroscopic bioconvectivepatterns to measure the toxic response, giving asensitivity better than 1 u.g/1 and a toxicitythreshold to 7 ug/1 for Cd+2. Cadmium hinderspattern formation in a dose-dependent manner.Arrested organism growth arises from sloweddivision and mutation to nondividing classes.Unlike previous efforts, this method can be per-formed in a shallow flow device and does notrequire electronic or chemical analyses tomonitor toxicity.

TM-103524 January 1991An Evaluation of Bearings Operating in aCryogenic Environment With Silicon NitrideRolling Elements, H.G. Gibson. Materialsand Processes Laboratory. N91 -18436

The bearings used in the space shuttle mainengine (SSME) high pressure oxidizer turbo-pump (HPOTP) do not meet the expected lifegoals that were set for them. In an effort toimprove their performance, many solutions arebeing studied. New bearing materials are beingdeveloped, better manufacturing techniques arebeing investigated, and improved cage materialsfor better lubrication are being tested. This reportfocuses on the replacement of steel balls with

Page 9: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

ones made of silicon nitride in 57-mm HPOTPbearings. The bearings were then installed in atest rig and run at near turbopump operatingconditions. The results from this test series havebeen encouraging, with silicon nitride showinggood wear resistance and thermal stability.

TM-103525 November 1990Atmospheric Environment for Space Shuttle(STS-41) Launch. G.L. Jasper and G.W.Batts. Space Science Laboratory.

N91-19529

This report presents a summary of selectedatmospheric conditions observed near spaceshuttle STS-41 launch time on October 6, 1990,at Kennedy Space Center, Florida. Values ofambient pressure, temperature, moisture, groundwinds, visual observations (cloud), and windsaloft are included. The sequence of prelaunchJimsphere-measured vertical wind profiles isgiven in this report. The final atmospheric tape,which consists of wind and thermodynamicparameters versus altitude, for STS-41 vehicleascent has been constructed. The STS-41 ascentatmospheric data tape has been constructed byMarshall Space Flight Center's Earth Scienceand Applications Division to provide aninternally consistent data set for use in postflightperformance assessments and represents thebest estimate of the launch environment to the400,000-ft altitude that was traversed by theSTS-41 vehicle.

TM-103526 February 1991A Damage Tolerance Comparison ofIM7/8551 and IM8G/8553 Carbon/EpoxyComposites. D.G. Lance and A.T. Nettles.Materials and Processes Laboratory.

N91-18222

A damage tolerance study of two newtoughened carbon fiber/epoxy resin systems wasundertaken as a continuation of ongoing workinto screening new opposites for resistance toforeign object impact. This report is intended tobe a supplement to NASA TP 3029 in which fournew fiber/resin systems were tested for damagetolerance. Instrumented drop weight impacttesting was used to inflict damage to 16-plyquasi-isotropic specimens. Instrumented outputdata and cross-sectional examination of thedamage zone were utilized to quantify thedamage. It was found that the two fiber/resin

systems tested in this study were much moreimpact resistant than an untoughened compositesuch as T300/934, but were not as impact resis-tant as other materials previously studied.

TM-103527 March 1991Evaluation of Bearing Configurations Usingthe Single Bearing Tester in Liquid Nitrogen.T. Jett, P. Hall, and R. Thorn. Materials andProcesses Laboratory. N91-21532

Various bearing configurations were testedusing the Marshall Space Flight Center singlebearing tester with LN2 as the cryogenic coolant.The baseline was one Rocketdyne phase I highpressure oxidizer turbopump (HPOTP) pump end45-mm bore bearing. The bearing configurationsthat were tested included a Salox/M cage con-figuration, a silicon nitride ball configuration, anelongated cage configuration, and a Bray 601grease configuration.

TM-103528 February 1991GEOSIM—A Numerical Model for Geo-physical Fluid Flow Simulation. Karen A.Butler, Timothy L. Miller, and Huei-Iin Lu.Space Science Laboratory. N91-21450

A numerical model which simulates geo-physical fluid flow in a wide range of problems isdescribed in detail, and comparisons of some ofthe model's results are made with previousexperimental and numerical studies. The modelis based upon the Boussinesq Navier-Stokesequations in spherical coordinates, which can bereduced to a cylindrical system when latitudinalwalls are used near the pole and the ratio oflatitudinal length to the radius of the sphere issmall. The equations are approximated by finitedifferences in the meridional plane and spectraldecomposition in the azimuthal direction. Theuser can specify a variety of boundary and initialconditions, and there are five different spectraltruncation options. The results of five validationcases are presented: (1) the transition betweenaxisymmetric flow and baroclinic wave flow inthe side-heated annulus; (2) the steady baro-clinic wave of the side-heated annulus; (3) thewave-amplitude vacillation of the side-heatedannulus; (4) transition to baroclinic wave flow ina bottom-heated annulus; and (5) the SpacelabGeophysical Fluid Flow Cell (spherical)experiment.

Page 10: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

TM-103529 March 1991An Evaluation of GTAW-P Versus GTAWelding of Alloy 718. W.R. Gamwell, C.Kurgan, and T.W. Malone. Materials andProcesses Laboratory. N91-21287

Mechanical properties have been evaluatedto determine statistically whether the pulsedcurrent gas tungsten arc welding (GTAW-P)process produces welds in alloy 718 with roomtemperature structural performance equivalent tocurrent space shuttle main engine (SSME)welds manufactured by the constant current gastungsten arc welding (GTAW) process.Evaluations were conducted on two base metallots, two filler metal lots, two heat input levels,and two welding processes. The material formwas 0.125-inch (3.175-mm) alloy 718 sheet.Prior to welding, sheets were heat treated toeither the ST or STA-1 condition. After welding,panels were left as welded or heat treated to theSTA-1 condition, and weld beads were left intactor machined flush. Statistical analyses wereperformed on yield strength (YS), ultimate ten-sile strength (UTS), and high cycle fatigue(HCF) properties for all the post weldedmaterial conditions. Analyses of variance(ANOVA) were performed on the data todetermine if there were any significant effects onUTS or HCF life due to variations in base metal,filler metal, heat input level, or welding process.

Statistical analyses have shown that theGTAW-P process does produce welds withroom temperature structural performanceequivalent to current SSME welds manufacturedby the GTAW process, regardless of priormaterial condition or post welding condition.

TM-103530 February 1991Atmospheric Environment for Space Shuttle(STS-38) Launch. G.L. Jasper and G.W.Batts. Space Science Laboratory.

N91-21633

This report presents a summary of selectedatmospheric conditions observed near spaceshuttle STS-38 launch time on November 15,1990, at Kennedy Space Center, Florida. STS-38carried a Department of Defense payload and theflight azimuth in this report will be denoted by areference flight azimuth, since the actual flightazimuth is not known. Values of ambient pres-sure, temperature, moisture, ground winds,visual observations (cloud), and winds aloft are

included. The sequence of prelaunch Jimsphere-measured vertical wind profiles is given in thisreport. The final atmospheric tape, which con-sists of wind and thermodynamic parametersversus altitude, for STS-38 vehicle ascent hasbeen constructed. The STS-38 ascent atmos-pheric data tape has been constructed byMarshall Space Flight Center's Earth Scienceand Applications Division to provide aninternally consistent data set for use in postflightperformance assessments and represents thebest estimate of the launch environment to the400,000-ft altitude that was traversed by theSTS-38 vehicle.

TM-103531 April 1991NASA Marshall Space Flight Center SolarObservatory Report—July-September 1990.James E. Smith. Space Science Laboratory.

N91-22951

This report provides a description of theNASA Marshall Space Flight Center's SolarVector Magnetograph Facility and gives a sum-mary of its observations and data reduction dur-ing July-September 1990. The systems thatmake up the facility are a magnetograph tele-scope, an H-alpha telescope, a Questar tele-scope, and a computer code. The data are repre-sented by longitudinal contours with azimuthplots.

TM-103532 April 1991NASA Marshall Space Flight Center SolarObservatory Report—October-December1990. James E. Smith. Space ScienceLaboratory. N91-22952

This report provides a description of theNASA Marshall Space Flight Center's SolarVector Magnetograph Facility and gives a sum-mary of its observations and data reduction dur-ing October-December 1990. The systems thatmake up the facility are a magnetograph tele-scope, an H-alpha telescope, a Questar tele-scope, and a computer code. The data are repre-sented by longitudinal contours with azimuthplots.

TM-103533 May 1991An Evaluation of the Total QualityManagement (TQM) Implementation Stra-tegy for the Advanced Solid Rocket MotorProject at NASA's Marshall Space Flight

Page 11: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

Center. Harry F. Schramm and Kenneth W.Sullivan. N91-24599

This document represents an evaluation ofthe NASA's Marshall Space Flight Center(MSFC) strategy to implement total qualitymanagement (TQM) in the advanced solid rocketmotor (ASRM) project. The evaluation of theimplementation strategy reflected the CivilService personnel perspective at the projectlevel. The external and internal environments atMSFC were analyzed for their effects on theASRM TQM strategy. Organizational forms,cultures, management systems, problem solvingtechniques and training were assessed for theirinfluence on the implementation strategy. Theinfluence of ASRM's effort was assessed rela-tive to its impact on mature projects as well asfuture projects at MSFC.

TM-103534 April 1991Parametric Study in Weld Mismatch ofLongitudinally Welded SSME HPFTP Inlet.J.B. Min, K.L. Spanyer, and R.M. Brunair.Structures and Dynamics Laboratory.

N91-23502

Welded joints are an essential part ofpressure vessels such as the space shuttle mainengine (SSME) turbopumps. Defects produced inthe welding process can be detrimental to weldperformance. Recently, review of the SSME highpressure fuel turbopump (HPFTP) titanium inletx rays revealed several weld discrepancies suchas penetrameter density issues, film processingdiscrepancies, weld width discrepancies,porosity, lack of fusion, and weld offsets.Currently, the sensitivity of welded structures todefects is of concern. From a fatigue standpoint,weld offset may have a serious effect since localyielding, in general, aggravates cyclic stresseffects. Therefore, the weld offset issue is con-sidered in this report. Using the finite elementmethod and mathematical formulations, para-metric studies were conducted to determine theinfluence of weld offsets and a variation of weldwidths in longitudinally welded cylindricalstructures with equal wall thicknesses on bothsides of the joint. From the study, the finite ele-ment results and theoretical solutions are pre-sented.

TM-103535 April 1991Effects of Water on the Strength of Zerodur.D. Tucker and A. Setzer. Materials andProcesses Laboratory. N91-24430

An experimental design matrix was con-structed to determine the effects of time andtemperature water soak on the strength ofZerodur glass-ceramic. It was found thatstrength does increase in a nonlinear mannerwhich is consistent with existing theories ofcrack tip blunting and residual stress reduction.

TM-103536 May 1991Effect of Flange Bolt Preload on SpaceShuttle Main Engine High Pressure OxidizerTurbopump Housing Analysis. J.B. Min, L.M.Johnston, and B. Czekalski. Structures andDynamics Laboratory. N91-245 84

Cracks at the seal fillet flange and the strutpilot groove of primary turbine drain passage ofthe space shuttle main engine (SSME) highpressure oxidizer turbopump (HPOTP) havebeen observed and reported. Stress informationfor critical structural components in the SSMEunder actual conditions is necessary for designand life prediction analysis. However, littleinformation is available about the stress distri-bution at this location under various combina-tions of loadings and environments. Thus, astress analysis was conducted to determine aninfluence of the various operation and installationloads on the stresses of the HPOTP mainmounting flange. To do this, a three-dimensional(3-D) finite element model of the HPOTP hous-ing was generated. A fairly comfortable margin ofstresses at the flange fillet with respect to theyield stress of Inconel 718 is shown in thisanalysis. However, it was revealed that thebending stress arising from the housing flangebolt preloads could significantly affect the stressdistribution at the strut pilot groove of primaryturbine drain passage in the HPOTP housing.Consequently, the information obtained from thepresent 3-D analysis results should be useful inguiding the development of the SSME HPOTP.

TM-103537 May 1991The Effect of Stress on Hydrogen Uptake andDesorption by A-286. M.D. Danford.

. Materials and Processes Laboratory.N91-28341

Page 12: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

The uptake and desorption of hydrogen byA-286 as a function of stress has been studiedusing electrochemical methods. It was found thatthe apparent surface hydrogen concentration C0,the mean hydrogen concentration C, and thehydrogen distribution uniformity all increased upto a stress level 50-percent of yield anddecreased thereafter. The value of the hydrogendiffusion coefficient D was relatively unaffectedby stress while the percent of trapped hydrogenappeared to decrease with increasing stress.

TM-103538 June 1991Atmospheric Environment for Space Shuttle(STS-35) Launch. G.L. Jasper and G.W.Batts. Space Science Laboratory.

N91-25550

This report presents a summary of selectedatmospheric conditions observed near spaceshuttle STS-35 launch time on December 2,1990, at Kennedy Space Center, Florida. Valuesof ambient pressure, temperature, moisture,ground winds, visual observations (cloud), andwinds aloft are included. The sequence ofprelaunch Jimsphere-measured vertical windprofiles is given in this report. The finalatmospheric tape, which consists of wind andthermodynamic parameters versus altitude, forSTS-35 vehicle ascent has been constructed.The STS-35 ascent atmospheric data tape hasbeen constructed by Marshall Space FlightCenter's Earth Science and Applications Divisionto provide an internally consistent data setfor use in postflight performance assessmentsand represents the best estimate of the launchenvironment to the 400,000-ft altitude that wastraversed by the STS-35 vehicle.

TM-103539 April 1991Analysis of Lightning Field ChangesProduced by Florida Thunderstorms. W.J.Koshak. Space Science Laboratory.

N91-25555

A new method is introduced for inferring thecharges deposited in a lightning flash. Previousnonlinear least-squares methods have usedsimple point charge (Q) and point dipole (P)models to describe ground-based observationsof lightning-caused field changes (AFs). In thenew approach, the AE's are described by a moregeneral volume charge distribution that is definedon a large cartesian grid system centered above

the measuring network. We show that a linearsystem of equations can be used to relate theAE's at the ground to the values of charge on thisgrid. With this approach, it is possible to applymore general physical constraints to the chargesolutions, and it is possible to access theinformation content of the AE data. Computer-simulated AE inversions show that the locationand symmetry of the charge retrievals areusually consistent with the known test sources.Analyses of three natural lightning events showthat the linear method provides sourcedistributions that are in reasonable agreementwith Q- and P-model results.

TM-103540 June 1991The Corrosion Protection of 2219-T87Aluminum by Anodizing. M.D. Danford.Materials and Processes Laboratory.

N91-26312

Various types of anodized coatings havebeen studied for 2219-T87 aluminum. Theseinclude both type II and type III anodize coatswhich have been water sealed and a newlydeveloped and proprietary Magnaplate HCR™coat. Results indicate that type III anodizing isnot much superior to type II anodizing as far ascorrosion protection for 2219-T87 aluminum isconcerned. Magnaplate HCR™ coatings shouldprovide superior corrosion protection over anextended period of time using a coating thicknessof 51 microns (2.0 mils).

TM-103541 June 1991Illuminance and Luminance Distributions of aPrototype Ambient Illumination System forSpace Station Freedom. R.C. Mullican andB.C. Hayes. Mission Operations Laboratory.

N91-26193

Preliminary results of research conducted inthe late 1970's indicate that perceptual qualitiesof an enclosure can be influenced by the distribu-tion of illumination within the enclosure.Subjective impressions such as spaciousness,perceptual clarity, and relaxation or tenseness,among others, appear to be related to differentcombinations of surface luminance. A prototypeindirect ambient illumination system wasdeveloped which will allow crew members toalter surface luminance distributions within anenclosed module, thus modifying perceptual cuesto match crew preferences. A traditional lensed

Page 13: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

direct lightning system was compared to theprototype utilizing the full-scale mockup of SpaceStation Freedom developed by Marshall SpaceFlight Center. The direct lensed system wasinstalled in the habitation module with theindirect prototype deployed in the U.S. laboratorymodule. Analysis centered on the illuminanceand luminance distributions resultant from thesesystems and the implications of variousluminaire spacing options. All test configurationswere evaluated for compliance with NASAStandard 3000, "Man-System IntegrationStandards."

TM-103542 June 1991Vacuum Vapor Deposition—A Spinoff ofSpace Welding Development. R.M. Poorman.Materials and Processes Laboratory.

N91-27330

A vapor deposition process has been definedthrough a spinoff effort of space weldingdevelopment. In this development for welding ina space environment, a hollow electrode wasused to add gas precisely at the welding arc.This provides gas for ionization which carries thewelding arc current. During this weldingdevelopment metal vapor coatings wereobserved. These coatings are unique in that theyare produced by a new process. This reportcharacterizes some coatings produced and thepotential of this new and innovative vapordeposition process. Advantages over prior artare discussed.

TM-103543 June 1991Proof Test Diagrams for Zerodur Glass-Ceramic. D.S. Tucker. Materials andProcesses Laboratory. N91 -27332

Proof test diagrams for Zerodur glass-ceramic are calculated from available fracturemechanics data. It is shown that the environmenthas a large effect on minimum time-to-failure aspredicted by proof test diagrams.

TM-103544 June 1991Applications of Low Lift to Drag RatioAerobrakes Using Angle of Attack Variationfor Control. J.A. Mulqueen. PreliminaryDesign Office. N91 -28189

angle-of-attack variation for control. Theseapplications are: return from geosynchronous orlunar orbit to low Earth orbit and planetary aero-capture at Earth and Mars. A number of aero-brake design considerations are reviewed. It wasfound that the flow impingement behind theaerobrake and the aerodynamic heating loads arethe primary factors that control the sizing of anaerobrake. The heating loads and other loads,such as maximum acceleration, are determinedby the vehicle ballistic coefficient, theatmosphere entry conditions, and the trajectorydesign. Several formulations for defining an opti-mum trajectory are reviewed, and the variousperformance indices that can be used are evalu-ated. The "nearly grazing" optimal trajectorywas found to provide the best compromisebetween the often conflicting goals of minimizingthe vehicle propulsive requirements and min-imizing vehicle loads. The relationship betweenvehicle and trajectory design is investigated fur-ther using the results of numerical simulations oftrajectories for each aerobrake application. Thedata show the sensitivity of the trajectories toseveral vehicle parameters and atmosphericdensity variations. The results of the trajectoryanalysis show that low lift to drag ratio aero-brakes, which use angle-of-attack variationfor control, can potentially be used for a widerange of aerobrake applications.

TM-103546 July 1991BATSE-GRO Observations of Bremsstrah-lung from Electron Precipitation Events. J.M.Horack and G.J. Fishman. Space ScienceLaboratory.

The Burst and Transient Source Experiment(BATSE) on the Gamma Ray Observatory(GRO) has detected a large number of terrestrialelectron precipitation events. Bremsstrahlung isgenerated as the precipitating electrons interactin the atmosphere, or at the spacecraft, and thisradiation is detected by the gamma ray detectorsonboard. Several examples of such events arepresented here, and the different classes ofevents are described. A correlation of events tostrong magnetospheric activity is presented, andthe association of a subset of events to apowerful VLF transmitter on the western coastof Australia is described.

This report investigates several applicationsof low lift to drag ratio aerobrakes which use

Page 14: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

TM-103547 July 1991A Simulation of the Instrument System forthe Astro-1 Mission. M. Whorton, M. West,and J. Rakoczy. Structures and DynamicsLaboratory. N91-30061

NASA has recently completed a shuttle-borne stellar ultraviolet astronomy missionknown as Astro-1. A three-axis instrumentpointing system (IPS) was employed to accu-rately point the science instruments. In order toanalyze the pointing control system and verifypointing performance, a simulation of the IPS hasbeen developed using the multibody dynamicssoftware TREETOPS. The TREETOPS IPSsimulation is capable of accurately modeling themultibody IPS system undergoing large angle,nonlinear motion. This report documents thesimulation and presents example casesdemonstrating disturbance rejection, fine pointingoperations, and multiple target pointing andslewing of the IPS.

TM-103548 July 1991STS-35 Scrub 3 Hydrogen Leak Analysis. D.Seymour. Propulsion Laboratory.

During the summer of 1990, space shuttleColumbia experienced both an externaltank/orbiter disconnect hydrogen leak and mul-tiple internal aft compartment hydrogen leaks.After the third scrub of STS-35, a leak investi-gation team was organized. In support of thisteam, an analysis of the data obtained duringscrub 3 was performed. Based on this analysis,the engine 2 prevalve was concluded to be themost likely leak location and to account for mostof the observed leakage.

TM-103549 July 1991Evaluation of Chemical Conversion andSulfuric Acid Type II Anodize Coatings on7075-T73 and 2219-T87 Aluminum Alloys.V.C. McMillan. Materials and ProcessesLaboratory.

Corrosion evaluation studies were conductedon chemical conversion coated and anodized7075-T73 and 2219-T87 aluminum alloys. Thecorrosive environments ranged from a 95-percentrelative humidity combined with 35 °C (95 °F) toa 5-percent salt fog environment at 35 °C(95 °F). An evaluation of the effect of tempera-ture on corrosion protection and adhesion prop-

erties was conducted by exposing test samplesto various temperatures for specified timeperiods followed by environmental exposure andadhesion testing.

TM-103550 July 1991Empirical Predictions of HypervelocityImpact Damage to the Space Station. W.K.Rule and K.B. Hayashida. Structures andDynamics Laboratory.

This report describes a family of user-friendly, DOS PC based, Microsoft BASIC pro-grams written to provide spacecraft designerswith empirical predictions of space debrisdamage to orbiting spacecraft. The spacecraftwall configuration is assumed to consist ofmultilayer insulation (MLI) placed between aWhipple style bumper and the pressure wall.Predictions are based on data sets of experi-mental results obtained from simulating debrisimpacts on spacecraft using light gas guns onEarth. A module of the program facilitates thecreation of the data base of experimental resultsthat are used by the damage prediction modulesof the code. The user has the choice of threedifferent prediction modules to predict damage tothe bumper, the MLI, and the pressure wall. Oneprediction module is based on fitting low orderpolynomials through subsets of the experimentaldata. Another prediction module fits functionsbased on nondimensional parameters through thedata. The last prediction technique is a uniqueapproach that is based on weighting theexperimental data according to the distance fromthe design point.

TM-103551 July 1991Electrodeposited Zinc-Nickel as an Alter-native to Cadmium Plating for AerospaceApplication. V.C. McMillan. Materials andProcesses Laboratory.

Corrosion evaluation studies were conductedon 4130 alloy steel samples coated with elec-trodeposited zinc-nickel and samples coatedwith electrodeposited cadmium. The zinc-nickelwas deposited by the selection electrochemicalmetallizing process. These coated samples wereexposed to a 5-percent salt fog environment at35±2 °C (95±5 °F). The exposure period rangedfrom 96 to 240 hours. An evaluation of the effectof dichromate coatings on the performance ofeach plating was conducted. The protection

Page 15: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

afforded by platings with a dichromate seal wascompared to platings without the seal. Duringthe later stages of testing, deposit adhesion andpotential for hydrogen entrapment were alsoevaluated.

TM-103552 August 1991Multiplexing Readout Channels in Propor-tional Counters. J. Caristi. Space ScienceLaboratory.

Proportional counters are important instru-ments used in sensing "hard" x rays. Thisdocument describes the possibility of doublingthe number of readout channels in the detectorwithout increasing the electronics needed toamplify channel signals. This suggests that itshould be possible, conversely, to reduce thenumber of amplifiers, thereby reducing the weightand energy budget of the instrument. Variousnumerical multiplexing schemes are analyzed,and a computer program is presented that canreconstruct multiplexed channel outputs withvery good accuracy.

TM-103553 September 1991Materials and Processes Laboratory Com-posite Materials Characterization Task, PartI. Damage Tolerance. A.T. Nettles, D.S.Tucker, W.J. Patterson, S.W. Franklin, G.H.Gordon, L. Hart, A.J. Hodge, D.G. Lance,and S.S. Russel. Materials and ProcessesLaboratory.

In an effort to best utilize all areas of exper-tise within the Materials and ProcessesLaboratory, a Composite Materials Charac-terization Task Team was developed to helpbring together the various branches within theLaboratory to develop a comprehensive database on composite materials. A "test run" wasperformed on IM6/3501-6 carbon/epoxy in whichthe material was processed, machined intospecimens, and tested for damage tolerancecapabilities. Nondestructive test data played amajor role in this element of composite charac-terization. A time chart was produced showingthe time the composite material spent withineach Branch or Division in order to identify thoseareas which produce a long turnaround time.Instrumented drop weight testing was performedon the specimens with nondestructive evaluation(NDE) being performed before and after theimpacts. Destructive testing in the form of cross-

sectional photomicrography and compression-after-impact (CAI) testing were used. Resultsshow that the processing and machining stepsneeded to be performed more rapidly if data on acomposite material is to be collected within areasonable timeframe. The results of the damagetolerance testing showed that IM6/3501-6 is abrittle material that is very susceptible to impactdamage.

TM-4268, Part I April 1991The NASA/MSFC Global Reference Atmos-pheric Model—1990 Version (GRAM-90),Part I: Technical/Users Manual. C.G. Justus,F.N. Alyea, D.M. Cunnold, W.R. Jeffries m,and D.L. Johnson. Space Science Laboratory.

N91-26654

A new (1990) version of the NASA/MSFCGlobal Reference Atmospheric Model (GRAM-90) is presented and discussed. GRAM-90incorporates extensive new data, mostlycollected under the Middle Atmosphere Program(MAP), to produce a completely revised middleatmosphere model (20 to 120 km). Because ofearlier data sparseness in this altitude region,previous versions of GRAM relied on a 6-monthdisplacement of Northern Hemisphere data torepresent the Southern Hemisphere. GRAM-90alleviates this shortcoming by utilizing actualdata from the Southern Hemisphere for eachmonth. The NASA Marshall EngineeringThermosphere (MET) model has also beenincorporated into the GRAM-90 program, at allorbital altitudes greater than 120 km. Part I ofthis report serves as a technical description ofthe GRAM-90 program, with extensive docu-mentation on the program operation and usage.Sample results are presented, in the form ofheight-latitude and latitude-longitude plots.Comparisons are made between the empiricallybased GRAM-90 model and results from a "firstprinciples" stratospheric circulation model(SCM) in the 20- to 80-km height region.Specific areas of improvement of GRAM-90 overthe earlier GRAM model results are also noted.A test case example is also included. Part n ofthis report presents the entire GRAM-90 pro-gram listing along with the major data base list-ings.

TM^268, Part II April 1991The NASA/MSFC Global Reference Atmos-pheric Model—1990 Version (GRAM-90),

10

Page 16: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL MEMORANDUM

Part II: Program/Data Listings. C.G. Justus,F.N. Alyea, D.M. Cunnold, W.R. Jeffries ffl,and D.L. Johnson. Space Science Laboratory.

N91-27697

A new (1990) version of the NASA/MSFCGlobal Reference Atmospheric Model (GRAM-90) has been completed and the program and keydata base listings are presented in this docu-ment. GRAM-90 incorporates extensive newdata, mostly collected under the MiddleAtmosphere Program (MAP), to produce a com-pletely revised middle atmosphere model (20-120 km). At altitudes greater than 120 km,GRAM-90 uses the NASA MarshallEngineering Thermosphere (MET) model. Thisreport (part II) serves as a supplementary reportto the technical document of GRAM-90 (part I).Complete listings of all program and major databases are presented herein. Also, a test caseexample is included.

TM-4289 May 1991Atmospheric Turbulence Review of SpaceShuttle Launches. M. Susko. Space SciencesLaboratory. N91-23215

The primary objective of this paper is toreport on the research and analysis on identifyingturbulent regions from the surface to 16 km forspace shuttle launches. This research hasdemonstrated that the results from the FPS-16radar/jimsphere balloon system in measuringwinds can indeed indicate the presence or con-ditions ripe for turbulence in the troposphere andlower stratosphere. It is further demonstratedthat atmospheric data obtained during the shuttlelaunches by the rawinsonde in conjunction withthe jimsphere provides the necessary meteoro-

logical data to compute aerodynamic parametersto identify turbulence, such as Reynolds number,drag coefficient, turbulent stresses, total energy,stability parameter, vertical gradient of kineticenergy, Richardson number, and the turbulenceprobability index. There is no magic fool-proofcriteria in atmospheric turbulent probability ofoccurrence. However, enhanced temperaturelapse rates and inversion rates, strong vectorwind shears, and large changes in wind directionidentify the occurrence of turbulence at thetropopause. When any two of the above condi-tions occur simultaneously, a significant proba-bility of turbulence can occur as shown in thispaper.

TM-4301 June 1991The QDP/PLT User's Guide. A.F. Tennant.Space Science Laboratory.

N91-25682

PLT is a high level plotting package. AProgrammer can create a default plot suited forthe data being displayed. At run times, users canthen interact with the plot overriding any or all ofthese defaults. The user is also provided thecapability to fit functions to the displayed data.This ability to display, interact with, and to fit thedata make PLT a useful tool in the analysis ofdata. The Quick and Dandy Plotter (QDP) pro-gram will read ASCII text files that contain PLTcommands and data. Thus, QDP provides aneasy way to use the PLT software. QDP filesprovide a convenient way to exchange data. TheQDP/PLT software is written in standardFortran 77 and has been ported to VAX VMS,SUN UNIX, IBM AIX, NeXT NextStep, andMS-DOS systems.

11

Page 17: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL PAPERS

TP-3066 November 1990Electrochemical Studies of Corrosion In-hibitors. M.D. Danford. Materials and Pro-cesses Laboratory. N91-17208

The effect of single salts, as well as multi-component mixtures, on corrosion inhibition hasbeen studied for type 1010 steel; for 5052,1100,and 2219-T87 aluminum alloys; and for copper.Molybdate-containing inhibitors exhibit animmediate, positive effect for steel corrosion, butan incubation period may be required foraluminum before the effect of a given inhibitor canbe determined. The absence of oxygen was foundto provide a positive effect (smaller corrosionrate) for steel and copper, but a negative effectfor aluminum. This is attributed to the twopossible mechanisms by which aluminum canoxidize. Corrosion inhibition is generally similarfor oxygen-rich and oxygen-free environments.The results of this study show that the elec-trochemical method is an effective means ofscreening inhibitors for the corrosion of singlemetals, with caution to be exercised in the caseof aluminum.

TP-3075 January 1991Plate and Butt-Weld Stresses Beyond Elas-tic Limit, Material and Structural Modeling.V. Verderaime. Space Science Laboratory.

N91-16413

Ultimate safety factors of high performancestructures depend on stress behavior beyond theelastic limit—a region not too well understood.An analytical modeling approach was developedto gain fundamental insights into inelasticresponses of simple structural elements.Nonlinear material properties were expressed inengineering stresses and strains variables andcombined with strength of material stress andstrain equations similar to numerical piece-wiselinear method. Integrations are continuous whichallows for more detailed solutions. Included withinteresting results are the classical combinedaxial tension and bending load model and thestrain gauge conversion to stress beyond theelastic limit. Material discontinuity stress factorsin butt-welds were derived. This is a working-type document with analytical methods andresults applicable to all industries of high relia-bility structures.

TP-3108 March 1991A Novel Method of Testing the ShearStrength of Thick Honeycomb Composites.A.J. Hodge and A.T. Nettles. Materials andProcesses Laboratory. N91-21242

Sandwich composites of aluminum andglass/phenolic honeycomb core were tested forshear strength before and after impact damage.The assessment of shear strength was per-formed in two ways; by four-point bend testing ofsandwich beams and by a novel "double lapshear" (DLS) test. This novel testing techniquewas developed so smaller specimens could beused thus making the use of common laboratoryscale fabrication and testing possible. The twotechniques yielded similar data. The DLS testgave slightly lower shear strength values of thetwo methods but were closer to the supplier'svalues for shear strength.

TP-3123 June 1991A Scheme for Bandpass Filtering Magne-tometer Measurements to ReconstructTethered Satellite Skiprope Motion. M.E.Polites. Structures and Dynamics Labora-tory. N91-25629

This paper presents a unique scheme forreconstructing tethered satellite skiprope motionby ground processing of satellite magnetometermeasurements. The measurements are modifiedbased on ground knowledge of the Earth'smagnetic field and passed through bandpassfilters tuned to the skiprope frequency.Simulation results are presented which verify thescheme and show it to be quite robust. The con-cept is not just limited to tethered satellites.Indeed, it can be applied wherever there is aneed to reconstruct the coning motion of a bodyabout a known axis, given measurements of aknown vector in body-fixed axes.

TP-3128 August 1991The Interaction of Hydrogen With MetalAlloys. M.D. Danford and J.W. Montano.Materials and Processes Laboratory.

N91-29318

Hydrogen diffusion coefficients have beenmeasured for several alloys, and these havebeen determined to be about the same at 25 °Cfor all alloys investigated. The relation of struc-ture, both metallurgical and crystallographic, to

12

Page 18: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL PAPERS

the observed hydrogen distribution on charginghas been investigated, as well as the role ofhydride formation in the hydrogen resistance ofmetal alloys. An attempt has been made tocorrelate the structures and compositions ofmetals alloys as well as other parameters withthe ratios of their notched tensile strengths inhydrogen to that in helium, R(H2/He), which arebelieved to represent a measure of theirhydrogen resistance. Evidence supports thebelief that hydrogen permeability and hydrogenresistance are increased by smaller grain sizesfor a given alloy composition.

TP-3138 July 1991Nonlinear Viscoelastic Characterization andAnalysis Verification Program for SRMPropellant and Polymer Materials. C.J.Moore, R.F. Landel, S.T.J. Peng, and B.Marsh, Structures and Dynamics Laboratory.

X91-10616

The test program discussed in this reporthas potentially wide application to the testingand structural analysis of polymer materials andother materials generally characterized as beingmade of Viscoelastic materials. A joint NationalAeronautics and Space Administration, JetPropulsion Laboratory, and Army program of testand analysis has been established in order toprovide the nonlinear, Viscoelastic biaxialcharacterization of the structural and mechanicalproperties of the space shuttle solid rocket motor(SRM) propellant and the advanced solid rocketmotor (ASRM) propellant. This investigationwill also endeavor to obtain a consistent andcomplete set of propellant materials failure data.The data base and accompanying theoreticalcharacterization will be used to improve andrevise finite element modeling for shuttle andASRM-propellant motors.

TP-3139 August 1991Resource Envelope Concepts for MissionPlanning. K.Y. Ibrahim, J.D. Weiler, and J.C.Tokaz. Missions Operations Laboratory.

N91-29209

This document details seven proposedmethods for creating resource envelopesfor Space Station Freedom mission planning.Four reference science activity models are usedto illustrate the effect of adding operational flexi-bility to mission timelines. For each method, a

brief explanation is given along with graphs toillustrate the application of the envelopes to thepower and crew resources. The benefits andcosts of each method are analyzed in terms ofresource utilization. In addition to the effect onindividual activities, resource envelopes areanalyzed at the experiment level.

TP-3148 September 1991Stress Corrosion Study of Carburized AISI9310 and Carburized M-50 NiL Steels. P.O.Torres. Materials and Processes Laboratory.

A stress corrosion cracking (SCC) evalua-tion of Carburized AISI 9310 and Carburized M-50 NiL steels was undertaken. AISI 9310 is acandidate substitute to 440C for the bearinginner race in the space shuttle main enginealternate turbopump development program, andM-50 NiL may also find applications as a bear-ing alloy. Round tensile specimens of thesealloys at several stress levels, as well as corro-sion samples of AISI 9310, were exposed to100-percent relative humidity at 38 °C (100 °F).The maximum tensile stresses that produced noSCC failures in 1 year of exposure were 172 MPa(25 ksi) for AISI 9310 and 345 MPa (50 ksi) forM-50 NiL. Each AISI 9310 steel fractureshowed a circumferential crack between the caseand the core. Both alloys developed rust on thesurface and pitting; however, AISI 9310 rusted toa greater extent than M-50 NiL. Thin, densechrome (TDC) was also evaluated in this pro-gram as a corrosion barrier alternative; however,its protection was minimal. Corrosion spotsvisible to the naked eye appeared in less than 5days of exposure. Although TDC plating on testspecimens prevented the intensive corrosionattack which occurred in bare samples after along time exposure, the TDC plating did not offersufficient protection to avoid failures. The resultsobtained in this evaluation must be carefullyconsidered when designing bearing componentsmade of these materials.

TP-3161 September 1991Automating a Spacecraft Electrical PowerSystem Using Expert Systems. L.F. Lollar.Information and Electronic Systems Labora-tory.

Since Skylab, Marshall Space Flight Center(MSFC) has recognized the need for large elec-trical power systems (EPS's) in upcoming

13

Page 19: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA TECHNICAL PAPERS

spacecraft. The operation of the spacecraftdepends on the EPS. Therefore, it must be effi-cient, safe, and reliable. In 1978, as a conse-quence of having to supply a large number of EPSpersonnel to monitor and control Skylab, theElectrical Power Branch of MSFC began theautonomously managed power system (AMPS)project. This project resulted in the assembly of a25-kW high-voltage dc test facility and providedthe means of getting man out of the loop as muchas possible. AMPS includes several embeddedcontrollers which allow a significant level ofautonomous operation. More recently, the

Electrical Division at MSFC has developed thespace station module power management anddistribution (SSM/PMAD) breadboard toinvestigate managing and distributing power inthe Space Station Freedom habitation andlaboratory modules. Again, the requirement for ahigh level of autonomy for efficient operation overthe lifetime of the station and for the benefits ofenhanced safety has been demonstrated. Thispaper describes the two breadboards and thehierarchical approach to automation which wasdeveloped through these projects.

14

Page 20: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC CONFERENCE PUBLICATIONS

CP-3092 September 1990Advanced Earth-to-Orbit Propulsion Tech-nology—1990, Volume I of III. R.J. Richmondand S,T. Wu, Editors. X91-10285

CP-3092 September 1990Advanced Earth-to-Orbit Propulsion Tech-nology—1990, Volume II of III. R.J.Richmond and S.T. Wu, Editors. X91-10349

CP-3092 September 1990Advanced Earth-to-Orbit Propulsion Tech-nology— 1990, Volume III of III. R.J.Richmond and S.T. Wu, Editors. X91-10392

CP-3093 October 1990NASA/MSFC FY90 Global Scale Atmos-pheric Processes Research Program Review.F.W. Leslie, Editor. N91-16500

CP-3098 November 1990Paired and Interacting Galaxies—Interna-tional Astronomical Union Colloquium No.124. J.W. Sulentic, W.C. Keel, and C.M.Telesco, Editors. N91 -16850

CP-3119 May 1991The 1990 NASA Aerospace Battery Work-shop. L.M. Kennedy, Compiler.

CP-3126 September 1991NASA/MSFC FY91 Global Scale Atmos-pheric Processes Research Program Review.F.W. Leslie, Editor.

15

Page 21: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA REFERENCE PUBLICATIONS

RP-1262 May 1991 RP-1268 August 1991Methods of Applied Dynamics. M.H. Development of the Burst and TransientRheinfurth and H.B. Wilson. Structures and Source Experiment (BATSE). J.M. Horack.Dynamics Laboratory. N91-25303 Space Science Laboratory.

16

Page 22: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-4343 January 1991Hypervelocity Impact Physics. W.P.Schonberg, A.J. Bean, and K. Darzi. NAS8-36955. University of Alabama in Huntsville.

N91-19164

CR-4347 March 1991Theory of CW Lidar Aerosol BackscatterMeasurements and Development of a 2.1-\im Solid-State Pulsed Laser Radar forAerosol Backscatter Profiling. M.J. Kavaya,S.W. Henderson, and R.G. Frehlich. NAS8-37580. Coherent Technologies, Inc.

N91-19498

CR-184022 July 1990Single Crystal/Hollow Core Blades andNozzles for the SSME HPFTP—FinalReport. NAS8-40000. Rockwell Interna-tional. N90-91427

CR-184023 August 1990Final Report for the M-52 Spray BoothQualification Test. NAS8-30490. ThiokolCorp. N90-91432

CR-184024 June 1990Infrastructure Study Phase I Review (BASIC+ TD001-TD005). NAS8-37588. GeneralDynamics. X91-10060

CR-184025 July 1990Real-Time Failure Control (SAFD)—FinalReport. NAS8-40000. Rockwell Interna-tional. N91-11233

CR-184026 September 1990Flight Set 360L007 (STS-33R) Field JointProtection System, Thermal ProtectionSystem, and Systems Tunnel Components,Final Report—Volume VII. NAS8-30490.Thiokol Corp. N91-10115

CR-184027 September 1990Flight Motor Set 360H005 (STS-28R) FinalReport, Volume V, (Nozzle Component).NAS8-30490. Thiokol Corp. N91-12746

CR-184028 May 1990SEPAC Data Analysis in Support of theEnvironmental Interaction Program—InterimReport. NAS8-32488. Southwest ResearchInstitute. N91-13807

CR-184029 September 1990Space Shuttle Development Motor No. 9(DM-9) Final Test Report Volume 1.NAS8-30490. Thiokol Corp. N91-12747

CR-184030 June 1990Summary of Jaygo Mixing and FSM-1 Appli-cation of Castable Inhibitor and Liner FinalReport. NAS8-30490. Thiokol Corp.

N91-13569

CR-184031 August 1990Nova 201 Ultrasonic Thickness Gauge(Nova Gauge) Final Test Report. NAS8-30490. Thiokol Corp. N91-14581

CR-184032 July 1990Tethering Sockets and Wrenches FinalReport. NAS8-30490. Thiokol Corp.

N91-13675

CR-184033 J October 1990Microbial Ecology Laboratory ProceduresManual NASA/MSFC. NAS8-37814. Sver-drup Technology. N91-13856

CR-184034 July 1990Space Station Common Module NetworkTopology and Hardware Development—Final Report. NAS8-36583. Martin Marietta.

N91-14373

CR-184035 July 1990Space Station Automation of CommonModule Power Management and Distribu-tion, Interim Final Report. NAS8-36433.Martin Marietta. N91 -12748

CR-184036 August 1990Geostationary Platform Study AdvancedGeostationary Platform/Evolutionary SpaceStation Accommodation Study—FinalReport. NAS8-36103. Lockheed Missiles &Space Co., Inc. N91-12738

CR-184037 August 1990Geostationary Platform Study AdvancedESGP/Evolutionary S.S. Freedom Accom-modation Study. NAS8-36103. LockheedMissiles & Space Co., Inc. N91-12737

CR-184038 June 1990Effect of Boron on Intergranular Hot Crackingin Ni-Cr-Fe Superalloys Containing

17

Page 23: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

Niobium—Final Report. NAS8-38084.University of Alabama in Birmingham.

N90-26115

CR-184039 July 1990Modeling Limitations and Fine Structure inthe Neutral Upper Atmosphere, FinalReport. NAS8-36405. Smithsonian Institu-

' tion. X90-10076

CR-184040 March 1990Evaluation of Raytek Infrared Pyrometer forContinuous Propellant Temperature Mea-surement—Final Report. NAS8-30490.Thiokol Corp. N91-13570

CR-184041 September 1990Flight Motor Set 360L009 (STS-36) FinalReport Volume I—System Overview.NAS8-30490. Thiokol Corp. N91-12749

CR-184042 September 1990Space Transportation Engine Program(STEP) Phase B Design Concept ReviewMinutes. NAS8-38160. Rockwell Interna-tional.

CR-184043 September 1990Complete the Development and Constructionof a Spaceborne Hydrogen Maser Clock, forPeriod August 11, 1988 Through July 31,1990. NAS8-37752. Smithsonian Institution.

N91-31688

CR-184044 Octoberl990Research Reports—1990 NASA/ASEESummer Faculty Fellowship Program, FinalReport. NGT-01-002-099. The University ofAlabama in Tuscaloosa and The Universityof Alabama in Huntsville. N91-18967

CR-184045 September 1990Tropical Pacific Moisture Variability: ItsDetection, Synoptic Structure, and Conse-quences in the General Circulation. NAS8-37284. Texas A&M University. N91-13832

CR-184046 December 1989Application of Dynamical Systems Theory toGlobal Weather Phenomena—Final ReportSeptember 30, 1985 to December 1, 1989.NAS8-36356. Yale University. N91-91591

CR-184047 February 1990Annual Report for Work Completed UnderNAS8-36718 for the Period October-September 1988/89. NAS8-36718. Univer-sity of Alabama in Huntsville.

CR-184048 October 1990Material STE Process Protocol andChecklist, Final Report Task Area 4.1Design Methodology Shortfall, NASA SPIPBondlines. NAS8-37802. Science Applica-tions International Corp. X91-10063

CR-184049 August 1990Solid Rocket Motor (SRM) Bondline InitialIntegrated Process Failure Modes andEffects Analysis (PFMEA) Report (GenericVersion) Task Area 4.2. NAS8-37802.Science Applications International Inc.

X91-10062

CR-184050 August 1990Flight Set 360L006 STS-34 Field JointProtection System, Thermal ProtectionSystem, and Systems Tunnel ComponentsVolume IV, Final Report. NAS8-30490.Thiokol Corp. N91 -14415

CR-184051 August 1990Space Shuttle Redesigned Solid RocketMotor Certificate of Qualification (COQ)Data Report. NAS8-30490. Thiokol Corp.

N91-14416

CR-184052Telerobotic On-OrbitResupply System Final37743. SRS Technologies.

September 1990Remote FluidReport. NAS8-

N91-13474

CR-184053 September 1990Rocketdyne Phase III Verification Tests—Final Report for Task P315 for Peroid 3January 1990-1 September 1990. NAS8-38258. Metallurgy Research Facilities.

N91-70122

CR-184054 September 1990ATD Bearings—Final Report for Task P363Covering the Period 16 March 1990-1September 1990. NAS8-38258. IIT ResearchInstitute/MRF. N91-70126

18

Page 24: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184055 April 1990Quarterly Report for Period 1 February to 30April 1990. NAS8-38258. IIT ResearchInstitute/MRF. N91-90290

CR-184056 July 1990Quarterly Report HTRI-P06150-Q3, forPeriod May-July 1990. NAS8-38258.IIT Research Institute/MRF. N91-90291

CR-184057 July 1990Operation and Maintenance of MetallurgyResearch Facility Period 11-1-89-03-01-90.NAS8-38258. IIT Research Institute/MRF.

N91-90289

CR-184058 October 1990Summary of Non-Asbestos LinerDevelopment for NMASAM PropellantCartridge—Interim Report. NAS8-30490.Thiokol Corp. N91-70083

CR-184059 October 1990Vulcanized Repair of Asbestos NBRInsulation—Final Report. NAS8-30490.Thiokol Corp. N91-70089

CR-184060 September 1990Asbestos Floats Characterization—FinalReport. NAS8-30490. Thiokol Corp.

N90-70088

CR-184061 October 1990Characteristics of Trapped Proton Aniso-tropy at Space Station Freedom Altitudes.NAS8-37916. SAIC. N91-15953

CR-184062 October 1990Space Transportation Engine Program(STEP) Phase BE Progress Report July-September 1990. NAS8-38160. RockwellInternational. X91-10061

CR-184063 October 1990User's Manual for SCOOT. NAS8-37850.Dynetics, Inc. X91-10086

CR-184064 October 1990Final Report Under Contract Number NAS8-37098. Uwohali, Inc. N91-90731

CR-184065 October 1990Data Base Description and RetrievalProgram for the Trapped Proton Vector Flux

Data Bases VF1MAX and VF1MIN.NAS8-37916. Science Applications Inter-national Corp. N91-90902

CR-184066 July 1990The Evaluation of Uncured RTV in RSRMFlight Nozzle 10B, Final Report. NAS8-30490. Thiokol Corp. N91 -70263

CR-184067 August 1990Qualification of Flex Bearing Using Altax,Methyl Tuads, and Zinc Oxide From NewSources—Final Test Report. NAS8-30490.Thiokol Corp. N91-70308

CR-184068 April 1990Laser Atmospheric Wind Sounder(LAWS)—Final Study Report (Phase I)Volume I, Executive Summary. NAS8-37590. Lockheed Missiles & Space Co., Inc.

N91-17351

CR-184069 April 1990Laser Atmospheric Wind Sounder (LAWS)Final Study Report (Phase I) Volume II,Final Report. NAS8-37590. LockheedMissiles & Space Co., Inc. N91-17352

CR-184070 April 1990Laser Atmospheric Wind Sounder (LAWS)Final Study Report (Phase I) Volume in,Project Cost Estimates. NAS8-37590.Lockheed Missiles & Space Co., Inc.

N91-17353

CR-184071 May 1990Definition and Preliminary Design of theLaser Atmospheric Wind Sounder (LAWS)Phase I Final Report, Volume I, ExecutiveSummary. NAS8-37589. GE Astro SpaceDivision. N91-16332

CR-184072 May 1990Definition and Preliminary Design of theLaser Atmospheric Wind Sounder (LAWS)Phase I Final Report, Volume II. NAS8-37589. GE Astro Space Division. N91-16333

CR-184073 May 1990Definition and Preliminary Design of theLaser Atmospheric Wind Sounder (LAWS)Phase I Final Report, Volume III, Program

19

Page 25: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

Cost Estimates. NAS8-37589. GE AstroSpace Division. N91-16334

CR-184074 September 1990Scoping Estimates of the LDEF SatelliteInduced Radioactivity. NAS8-38427. ScienceApplications International Corp. N91-16056

CR-184075 May 1990Results of the Evaluation Effort for ExtrudingDL-1375 (Silica Filled EPDM) Factory JointWeatherseal Rubber Using a 6-inchExtruder Configuration. NAS8-30490.Thiokol Corp. N91-70273

CR-184076 November 1990Failure and Unsatisfactory ConditionSummary Report for the Space Shuttle SolidRocket Booster—Information RequirementsDocument. NAS8-36300. USBI. N91-90901

CR-184077 October 1990Technical Evaluation Motor No. 6 (TEM-6)Nozzle Final Test Report. NAS8-30490.Thiokol Corp. N91-70262

CR-184078 November 1990Space Shuttle Flight Support Motor No. 1(FSM-1) Final Test Report. NAS8-30490.Thiokol Corp. N91 -16064

CR-184079 October 1990Masking of Inhibitor Inside DiameterForward Surface During Liner Application.NAS8-30490. Thiokol Corp. N91-70450

CR-184080 November 1990Final Results of the 17A Nose Cap LDIInvestigation—Final Report. NAS8-30490.Thiokol Corp. N91-70261

CR-184081 November 1990Management and Display of Four-Dimensional Environmental Data Sets UsingMcIDAS, Final Report for Period 02-28-86-08-31-90. NAS8-36292. University ofWisconsin-Madison. N91-17579

CR-184082 February 1989An Inventory of Four-Dimensional DataSets for the Earth Sciences. NAS8-36292.University of Wisconsin-Madison.

N91-17434

CR-184083 November 1990Pressure Fed Thrust Chamber TechnologyProgram. NAS8-37365. GenCorp Aerojet.

N91-17135

CR-184084 November 1990Analysis of Wind Profile MeasurementsFrom an Instrumented Aircraft—InterimFinal Report. NAS8-37377. FWG Asso-ciates, Inc. N91-16523

CR-184085 September 1990Final Report on the Characterization of WeldRadiograph Enigma in 2219-T87 Aluminum.NAS8-37232. Auburn University.

N91-70311

CR-184086 December 1990Final Report for NAS8-35918. UniversitiesSpace Research Association. X91-91074

CR-184087 November 1990MNASA Evaluation of NARC-Supplied CCPRayon Precursor Material and NonasbestosInsulation and Liner Final Test Report.NAS8-30490. Thiokol Corp. N91-90903

CR-184088 March 1989Examination of Cracks in S/N 0000051 of the1U75161 Igniter Chamber—Final Report.NAS8-30490. Thiokol Corp. N91 -71674

CR-184089 November 1990Investigation Team Final Report—11AAFTPoor Liner Coverage—Final Report. NAS8-30490. Thiokol Corp. N91 -90909

CR-184090 November 1990Verification of the Improved M-52 AsbestosSifter/Shaker Final Report. NAS8-30490.Thiokol Corp. N91-90910

CR-184091 August 1990Flight Set 360L007 (STS-33) InsulationComponent Final Report Volume HI FinalRelease. NAS8-30490. Thiokol Corp.

N91-21230

CR-184092 December 1990RSRM-13 (360Q013) Final Report BallisticsMass Properties Flight Designation STS-41.NAS8-30490. Thiokol Corp. N91-17139

20

Page 26: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184093 December 1990Horizontal Field Joint Separation Fixture(H77-0450) Qualification Final Test Report.NAS 8-30490. Thiokol Corp. N91-90908

CR-184094 December 1990The Design and Development of the HubbleSpace Telescope Neutral Buoyancy Trainer.N AS 8-35 318. Essex Corp. N91 -17068

CR-184095 January 1991Rotating Reactor Studies—Final ReportPeriod Covered 03-27-89-09-27-90. H-80505B. Roberts Associates Inc. N91-15421

CR-184096 July 1987Final Report on the Structural AssemblyDemonstration Experiment (SADE). NAS8-34959. MIT Space Systems Laboratory.

CR-184097 August 1986Selected Tether Applications in Space—Work Breakdown Structure (WBS) andWBS Dictionary (BASICS). NAS8-36616.Martin Marietta. N91-90907

CR-184098 August 1989Tether Deployment Monitoring System—SBIR Phase II Final Report. NAS8-37336.Anco Engineers. Inc.

CR-184099 February 1991Large Liquid Rocket Engine TransientPerformance Simulation System—FinalReport. NAS8-36994. United TechnologiesCorp. Pratt & Whitney. N91-21232

CR-184100 January 1991Blade Tip Rubbing Stress Prediction—FinalReport. NAS8-36361. Rockwell Interna-tional. N91-18435

CR-184101 January 1991Analysis of Rolling Contact Spall Life in440C Steel Bearing Rims—Final Report.NAS8-37764. Vanderbilt University.

N91-21526

CR-184102 December 1990Technology Development Program Plan forALS Liquid Fuel Turbopump AdvancedDevelopment Program Plan—Final Report.NAS8-37594. Rockwell International.

X91-10338

CR-184103 December 1990Spacelab System Analysis Advanced SolidRocket Motor (ASRM) CommunicationsNetworks Analysis—Final Report. NAS8-36717. Mississippi State University.

N91-18209

CR-184104 October 1990Flight Motor Set 360T010 (STS031R) FinalReport Volume I—System Overview.NAS8-30490. Thiokol Corp. N91-21231

CR-184105 December 1990Space Shuttle Production Verification Motor1 (PV-1) Field Joint Protection System FinalReport Volume VII. NAS8-30490. ThiokolCorp. N91-18208

CR-184106 November 1990TP-H1148 Knitline Integrity EvaluationFinal Report. NAS8-30490. Thiokol Corp.

N91-18288

CR-184107 January 1991RSRM-11 (360W011) Final ReportBallistics Mass Properties (STS-34).NAS8-30490. Thiokol Corp. N91-20203

CR-184108 January 1991Environmental Data Recorder (EDR)Qualification Final Test Report. NAS8-30490. Thiokol Corp. N91-18406

CR-184109 July 1990RSRM Top Hat Cover Simulator LightningTest Final Report—Volume 1. NAS8-30490.Thiokol Corp. N91 -22303

CR-184110 January 1991The Full-Scale Process and Design Changesfor Elimination of Insulation EdgeSeparations and Voids in the Tang FlapArea Final Report. NAS8-30490. ThiokolCorp. N91-19172

CR-184111 July 1990RSRM Top Hat Cover Simulator LightningTest Final Report—Volume II, Appendix.NAS8-30490. Thiokol Corp. N91-22304

CR-184112 December 1990Satellite Servicing Economic Study—Executive Summary. NAS8-38142. SpaceSystems/Loral. N91-19162

21

Page 27: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184113 December 1990Final Technical Report Satellite ServicingEconomic Study. NAS8-38142. SpaceSystems/Loral. N91-19163

CR-184114 January 1991Influence of a Magnetic Field DuringDirectional Solidification of MAR-M 246+HfSuperalloy—Final Report. NAS8-36461.University of Alabama at Birmingham.

N91-22416

CR-184115 December 1990LDEF Experiment P0006 Linear EnergyTransfer Spectrum Measurement (LETSME)Quick Look Report—Final Report. NAS8-38188. Eril Research Inc. N91-19223

CR-184116 July 1988Space Transportation Main Engine Reduced-Cost Configuration Study Phase A InterimReport. NAS8-36868. United TechnologiesPratt & Whitney. X91 -71839

CR-184117 March 1987Space Transportation Booster EngineConfiguration Study Preliminary Final Report(DR4) Executive Summary. NAS8-36857.United Technologies Pratt & Whitney.

CR-184118 March 1987Space Transportation Booster EngineConfiguration Study Preliminary Final Report(DR4) Includes Design Definition Document(DR8) and Environmental Analysis (DR10).NAS8-36857. United Technologies Pratt &Whitney.

CR-184119 March 1987Space Transportation Booster EngineConfiguration Study Preliminary Final Report(DR4) Program Cost Estimates (DR6) andWork Breakdown Structure and WBSDictionary (DR5). NAS8-36857. UnitedTechnologies Pratt & Whitney.

CR-184120 July 1987Space Transportation Main EngineConfiguration Study Preliminary Final Report(DR4) Includes Design Definition Document(DR8) and Environmental Analysis (DR10).NASS-36868. United Technologies Pratt &Whitney. X91-10284

CR-184121 July 1987Space Transportation Main EngineConfiguration Study—Preliminary FinalReport (DR-4) Program Cost Estimates(DR6) and Work Breakdown Structure andWBS Dictionary (DR5). NAS8-36868.United Technologies Pratt & Whitney.

CR-184122 January 1991Evaluation of the M-52 Dry Filter SprayBooth Final Report. NAS8-30490. ThiokolCorp. N91-70847

CR-184123 October 1990Follow-On Cable Coupling Lightning TestFinal Test Report Volume I. NAS8-30490.Thiokol Corp. N91-28192

CR-184124 October 1990Follow-On Cable Coupling Lightning TestFinal Report Volume II—Appendixes A, B,C, and D. NAS8-30490. Thiokol Corp.

N91-26195

CR-184125 October 1990Follow-On Cable Coupling Lightning TestFinal Test Report Volume III—AppendixesE and F. NAS8-30490. Thiokol Corp.

N91-27203

CR-184126 January 1991An Investigation of the Detection of TornadicThunderstorms by Observing Storm TopFeatures Using Geosynchronous SatelliteImagery. NAS8-38135. North Carolina StateUniversity. N91-20589

CR-184127 August 1990Liquid Rocket Booster Study Addendum toFinal Report. NAS8-37137. GeneralDynamics. N91-22368

CR-184128 February 1990Liquid Rocket Booster (LRB) for the SpaceTransportation System (STS) SystemsStudy, Volume II—Final Report Addendum1. NAS8-37136. Martin Marietta.

N91-22366

CR-184129 October 1990High Resolution Microwave SpectrometerSounder (HIMSS) Instrument Program—Final Report, Volume I, Book I, Executive

22

Page 28: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

Summary and Technical. NAS8-38175.Hughes Space and Communications Group.

N91-22542

CR-184130 October 1990High Resolution Microwave SpectrometerSounder (HIMSS) Instrument ProgramVolume I, Book 2, Preliminary ProgramPlans, CEI Specification Instrument InterfaceDescription Document. NAS8-38175.Hughes Space and Communications Group.

N91-22541

CR-184131 February 1991Flight Set 360L008 (STS-32) Case andSeals Final Report. NAS8-30490. ThiokolCorp. N91-71170

CR-184132 January 1991Turbopump Technology Validation TaskDefinitions—Final Report. NAS8-37593.GenCorp Aerojet. X91-10583

CR-184133 February 1991Addendum to Liquid Rocket Booster StudyFinal Report. NAS8-37137. GeneralDynamics. N91-71042

CR-184134 December 1990Spacelab Rack Lessons Learned—FinalReport. NAS8-32350. McDonnell Douglas.

N91-71034

CR-184135 February 1991Solid Propulsion Integrity Program NozzleSecond Annual Review "The Year ofFocusing the Thrust," Final Report VolumeI. NAS8-37801. Hercules Aerospace Co.

X91-10451

CR-184136 February 1991Solid Propulsion Integrity Program NozzleSecond Annual Review "The Year ofFocusing the Thrust," Final Report VolumeII. NAS8-37801. Hercules Aerospace Co.

X91-10452

CR-184137 January 1991Cosmic Ray Nuclei (CRN) DetectorInvestigation—Final Report. NAS8-32828.The University of Chicago. N91-22063

CR-184138 February 1991Engineering Support for an UltravioletImager for the ISTP Mission—Final Report.NAS8-37586. The University of Alabama inHuntsville. N91-22364

CR-184139 February 1991Physical Phenomena in Containerless GlassProcessing—Final Report. NAS8-32944.Clarkson University. N91-71157

CR-184140 March 19913Helium/4Helium Dilution Cryocooler forSpace—Final Report for July 12, 1989-February 12, 1991. NAS8-37437. AlabamaCryogenic Engineering, Inc. N91-20327

CR-184141 March 1991Solid Rocket Booster Internal Flow Analysisby Highly Accurate Adaptive ComputationalMethods—Final Report. NAS8-37682.Computational Mechanics Co., Inc.

N91-21239

CR-184142 March 1991Center Segment Tang Bulb Region ProposedChange Demonstration—Final Report.NAS8-30490. Thiokol Corp. N91 -71169

CR-184143 March 1991Early Focus Development Effort, UltrasonicInspection of Fixed Housing Metal-to-Adhesive Bondline Final Report. NAS8-30490. Thiokol Corp. N91 -22573

CR-184144 October 1990Propellant Tank Pressurization SystemTechnology Program—Volume I ExecutiveSummary. NAS8-37666. Martin Marietta.

N91-71037

CR-184145 October 1990Propellant Tank Pressurization SystemTechnology Program—Volume II, TechnicalReport. NAS8-37666. Martin Marietta.

N91-71041

CR-184146 October 1990Propellant Tank Pressurization SystemTechnology Program Appendix A, PropellantTank Pressurization System Flight ArticlePreliminary Requirements. NAS8-37666.Martin Marietta. N91-71153

23

Page 29: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184147 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix B,PTPSTP Technology Acquisition Plan.NAS8-37666. Martin Marietta. N91-71036

CR-184148 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix C,Task 1 Report: Catalytic Heating ofPressurant. NAS8-37666. Martin Marietta.

N91-71306

CR-184149 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix D,Aerojet Propulsion Division PTPSTP FinalReport. NAS8-37666. Martin Marietta.

N91-71152

.CR-184150 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix E,Flight Systems Trade Studies Summary.NAS8-37666. Martin Marietta. N90-71038

CR-184151 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix F,Flight Systems Optimization StudiesSummary. NAS8-37666. Martin Marietta.

N91-71039

CR-184152 October 1990Propellant Tank Pressurization SystemTechnology Program Volume II, Appendix G,Tank Pressurization Control System Study,Honeywell Space and Strategic Operations.NAS8-37666. Martin Marietta. N91-71040

CR-184153 April 1991MLIBLAST—A Program to EmpiricallyPredict Hypervelocity Impact Damage to theSpace Station. NAG8-123(10). University ofAlabama Tuscaloosa. N91-22363

CR-184154 February 1991Evaluation of Carbon-Carbon for SpaceEngine Nozzles, Phase II Final Report forSeptember 1988 to February 1991. NAS8-37684. GenCorp Aerojet X91-10283

CR-184155 March 1991Liquid Rocket Booster (LRB) for the SpaceTransportation System (STS) SystemsStudy Volume II—Final Report Addendum 2.NAS8-37136. Martin Marietta. N91-22374

CR-184156 October 1990The Ultra High Resolution XUVSpectroheliograph an Attached Payload forthe Space Station Freedom—Final Report.NAS8-38666. Stanford University.

N91-22365

CR-184157 January 1991Feasibility Study of the SuperconductingGravity Gradiometer (SGG) Flight Test onthe European Retrievable Carrier(EURECA)—Final Report. NAS8-38138.General Electric Co. N91-23229

CR-184158 March 1991Final Report NAS8-37592. Intersonics Inc.

N91-24558

CR-184159 October 1990RSRM Reliability Demonstration Report forthe Third Quarter 1990. NAS8-30490.Thiokol Corp. N91-71388

CR-184160 February 1991Management Quarterly Review, Final.NAS8-37802. Science Applications Inter-national Corp. X91-10511

CR-184161 April 1991Heavy Hydrocarbon Main InjectorTechnology Program—Final Report. NAS8-36369. Rockwell International. N91-21235

CR-184162 April 1991High Resolution Microwave SpectrometerSounder (HIMSS) Instrument ProgramAppendix: TRMM Study (A Radiometer forNASA's Tropical Rainfall MeasuringMission). NAS8-38175. Hughes Space andCommunications Group. N91-25548

CR-184163 April 1991Technical Evaluation Motor No. 7 (TEM-7)Final Test Report. NAS8-30490. ThiokolCorp. N91-26203

CR-184164 April 1991Final Report on NAS8-38436. TRW.

24

Page 30: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184165 December 1990Advanced Microwave Precipitation Radiom-eter (AMPR) for Remote Observation ofPrecipitation Final Report for Period 31December 1987-31 December 1990. NAS8-37142. Georgia Institute of Technology.

N91-26655

CR-184166 May 1991U.S. and Foreign Alloy Cross-ReferenceData Base. NAS8-36166. Fisk University.

N91-26313

CR-184167 April 1991Marshall Space Flight Center MicrogravityStrategic Plan—A Planning Exercise, FinalReport. NAS8-38669. Center for Space andAdvanced Technology. N91-24463

CR-184168 June 1990Surface Evaluation of HPOTP Bearing TestSet With Salox-M Cage. H-06865D.Wedeven Associates, Inc. X91-10584

CR-184169 March 1991Chemical Waste Disposal in Space byPlasma Discharge. NAS8-37195. TheUniversity of Alabama in Huntsville.

N91-29737

CR-184170 July 1991Activation Calculations for Trapped ProtonsBelow 200 MeV Appendix—Final TechnicalReport. NAS8-36649. Eastern KentuckyUniversity. N91-29865

CR-184171 July 1991Study of Activation of Metal Samples FromLDEF-1 and Spacelab-2—Final TechnicalReport. NAS8-36649. Eastern KentuckyUniversity. N91-29297

CR-184172 July 1990Space-Based Doppler Lidar SamplingStrategies—Algorithm Development andSimulated Observation Experiments—FinalReport. NAS8-37770. Simpson WeatherAssociates, Inc. N91-29554

CR-184173 October 1990Microgravity Science and ApplicationsVisiting Scientist Program—Final Report.NAS8-37366. Universities Space ResearchAssociation.

CR-184174 December 1989Final Report for Contract NAS8-36362March 4, 1987-September 15, 1989. NAS8-36362. The University of Alabama inHuntsville.

CR-184175 January 1990A Finite Element Solver for 3-DCompressible Viscous Flows. NAS 8-36555.The University of Tennessee Space Institute.

N91-29488

CR-184176 February 1990Process Validation for Lot AAF NozzleLSC's from JRC's North Carolina Facility,Final Test Report. NAS8-30490. ThiokolCorp. N91-71675

CR-184177 January 1990Lifting Beam Paint Investigation FinalReport. NAS8-30490. Thiokol Corp.

N91-71646

CR-184178 March 1991Space Transfer Concepts and Analysis forExploration Missions—Final Report. NAS8-37857. Boeing Defense & Space Group.

CR-184179 April 1989Systems Engineering Studies—Final Reporton NAS8-36955, Delivery Order No. 6. TheUniversity of Alabama in Huntsville.

N91-71676

CR-184180 April 1991Solid Propulsion Integrity Program NozzleQuarterly Management Review (FinalReport). NAS8-37801. Hercules AerospaceCo.

CR-184181 July 1991Studies in Remote Sensing of the Earth'sAtmosphere—Research Study: Final Report,Report Period October 6, 1987—March 15,1991. NAS8-37135. Universities SpaceResearch Association.

CR-184182 October 1990Design of a Large Subscale Solid RocketCombustion Simulator (LSSRCS) ForTesting SRM Nozzles. NAS8-37801.Hercules Aerospace Co.

25

Page 31: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184183 January 1991Attitude Profile Design Program—FinalReport. NAS8-37850. Dynetics, Inc.

CR-184184 February 1991Flight Set 360L007 (STS-33R) Case andSeal Final Report Volume II. NAS 8-30490.Thiokol Corp.

CR-184185 March 1991Aft Segment Dome-to-Stiffener FactoryJoint Insulation Void Elimination—FinalReport. NAS8-30490. Thiokol Corp.

CR-184186 February 1991Technical Evaluation Motor No. 7 (Tem-07)Interim Report (60 Day). NAS8-30490.Thiokol Corp.

CR-184187 September 1989Flight Motor Set 360T004 (STS-30R) FinalReport Volume I (System Overview).NAS 8-30490. Thiokol Corp.

CR-184188 July 1991SRB Seawater Corrosion Project—FinalReport. NAS8-38800. Auburn University.

CR-184189 July 1991Mechanism Test Bed Flexible Body Model

; Report. NAS8-38771. Control Dynamics Co.

CR-184190 May 1991Space Transportation Engine Program(STEP) Phase B—March Through April1991. NAS8-38160. Rockwell International.

CR-184191 March 1991Survey of Pressure Sensors for High-Temperature and High-AcousticEnvironments. NAS8-37801. HerculesAerospace Co.

CR-184192 April 1991Solid Rocket Combustion SimulatorNumerical Studies. NAS8-37801. HerculesAerospace Co.

CR-184193 January 1991Add-On to Nozzle Task 3.3.3.2 for "DX"Formulation Regression Rate Testing.NAS8-37801. Hercules Aerospace Co.

CR-184194 April 1991Solid Propulsion Integrity Program NozzleWork Package—Evaluation of HighTemperature Cements—Final Report.NAS8-37801. Hercules Aerospace Co.

CR-184195 October 1988Carbon Deposition Model for Oxygen-Hydrocarbon Combustion. NAS8-34715.Aerojet TechSystems Co.

CR-184196 April 1989Attachment 1 to Systems EngineeringStudies Report, NASA Reliability ManualStudy, Volume 1, Component Reliability.NAS8-36955. The University of Alabama inHuntsville.

CR-184197 April 1990Design and Analysis of Multilayer X-Ray/XUV Microscope—Final Report. H-805 89B. The University of Alabama inBirmingham.

CR-184198 June 1991Optimization Techniques Applied to PassiveMeasures for In-Orbit SpacecraftSurvivability: Interim Report. NAS8-37378.Science Applications International Corp.

CR-184199 June 1989Utilization of Satellite Cloud Information toDiagnose the Energy State andTransformations in Extratropical Cyclones,Final Report. NAS8-34009. PurdueUniversity.

CR-184200 September 1990A Study of Fracture Mechanisms in ATDRoller Bearing Final Report. NAS8-38083.Auburn University.

CR-184201 March 1991SEPAC Data Analysis in Support of theEnvironmental Interaction Program—FinalReport. NAS8-32488. Southwest ResearchInstitute.

CR-184202 March 1990Advanced Program Development Manage-ment Software System Final ReportSoftware Description and User's Manual.NAS8-36643. SRS Technologies.

26

Page 32: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

NASA CONTRACTOR REPORTS(Abstracts for these reports may be obtained from STAR)

CR-184203 March 1990Interactive Office User's Manual. NAS8-36643. SRS Technologies.

CR-184204 March 1990Evaluation of Advanced Propulsion Optionsfor the Next Manned Transportation SystemPropulsion Evolution Study—Final Report.NAS8-36643. SRS Technologies.

CR-184205 March 1990Evaluation of Undeveloped Rocket EngineCycle Applications to AdvancedTransportation Final Report. NAS8-36643.SRS Technologies.

CR-184206 December 1988Process Heat Energy for Lunar and MarsApplications—Task Final Report. NAS8-36643. SRS Technologies.

CR-184207 August 1991Engineering Cost Analysis and TechniquesDevelopment—Final Report. NAS8-36931.PRC, Inc.

CR-184208 May 1991Aero/Fluids Data Base System—FinalReport. NAS8-37463. Remtech.

CR-184209 June 1991Flow Induced Vibrations in the SSMEInjector Heads. NAS8-36195. RockwellInternational.

CR-184210 July 1991South Pacific Convergence Zone and Global-Scale Circulations, Final Report for Period 20July 1987-19 July 1991. NAS8-37127.Purdue University.

27

Page 33: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

ABBAS, M.M. ES55KUNDE, V.G.BRASUNAS, J.C.HERMAN, J.R.MASSIE, S.T.

Nighttime Reactive Nitrogen MeasurementsFrom Stratospheric Infrared ThermalEmission Observations. For publication inJournal of Geophysical Research,Washington, DC.

ABDELHAKJEM, W. ES75PATTERSON, J.D.LEHOCZKY, S.L.

A Comparison Between Electron Mobility inN-Type Hgi_xCdxTe and Hgi_xZnxTe. Forpublication in Materials Letters/MaterialsResearch Society, The Netherlands.

ADAMS, A.M. PT41Evolutionary Nuclear Thermal Rocketfor Manned Mars Missions. For presen-tation at AAS/AIAA AstrodynamicsSpecialist Conference, Durango, CO, August19-22,1991.

ANDERSON, D.M. EP55MOBLEY, T.B. Martin Marietta

Shuttle MPS—Test Simulator Project. Forpresentation at the AIAA 27th JointPropulsion Conference, Sacramento, CA,June 24, 1991.

ANDERSON, J.B. ED73Modal Survey Testing of the Lidar In-SpaceTechnology Experiment (LITE), a SpaceShuttle Payload. For presentation at theInternational Modal Analysis Conference,San Diego, CA, February 3-6, 1992.

ANDREWS, R.N. ES75PRICE, M.W.SU, C-H.SZOFRAN, F.R.LEHOCZKY, S.L.

The Effect of a Transverse Magnetic Field onthe Microstructure of Directionally SolidifiedCdTe. For presentation at the GordonConference, Plymouth, NH, July 15-19,1991.

APPLETON, P.N. ES65MARCUM, P.M.JOY, M.K.

Near-IR Observations of the Cartwheel RingGalaxy. For publication in ESO Messager,Garching, Germany.

ASAKIMORI, K. ES62BURNETT, T.H.CHERRY, M.L.CHRISTL, M.J.DAKE, S.DERRICKSON, J.H.FOUNTAIN, W.F.etal.

Three-Dimensional Simulations of Calorime-ter X-Ray Film Spots for Determining <Pj>.For presentation at the 22nd InternationalCosmic Ray Conference, Dublin, Ireland,August 11-23, 1991.

ASAKIMORI, K. ES62BURNETT, T.H.CHERRY, M.L.CHRISTL, M.J.DERRICKSON, J.H.FOUNTAIN, W.F.GREGORY, J.C.PARNELL, T.A.etal.

Energy Spectra of Proton and Helium NucleiAbove 5 TeV/Nucleaon. For presentation atthe 22nd International Cosmic RayConference, Dublin, Ireland, August 11-12,1991.

AUSTIN, R.E. PT01SUMRALL, J.P.HORSEWOOD, J.L.

NEP Options for the Early Phases ofManned Mars Exploration. For presentationat the Advanced SEI TechnologiesConference, Cleveland, OH, September 4-6,1991.

BABAI, M.K. EH44Mobile Robotic Hydroblast System. Forpresentation at the Sixth InternationalConference on CAD/CAM Robotics andFactories of the Future, London, U.K.,August 19-22, 1991.

28

Page 34: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

BACSKAY, A.S. ED62Space Station Freedom ECLSS DesignConfiguration: A Post Restructure Update.For presentation at the 21st IntersocietyConference on Environmental Systems, SanFrancisco, CA, July 15-18, 1991.

BAILEY, M. ED72BOWER, M.

Wings of the Sun: Long Duration Flight atHigh Altitude. For presentation at theSociety of Women Engineers 1991 NationalConvention and Student Conference, SanDiego, CA, June 24-29, 1991.

BALASUBRAMANIAM, K.S. ES52Blending Influence of Fe I 5250.6 A SpectralLine on the Fe I 5250.2 A Spectral Line andIts Implication for Polarization Measure-ments. For presentation at the AAS-SolarPhysics Division and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

BARBEE, T.W., JR. ES52HOOVER, R.B.et al.

The Multispectral Solar Telescope Array II:Soft X-Ray/EUV Reflectivity of theMultilayer Mirrors. For publication in OpticalEngineering, Bellingham, WA.

BAYGENTS, J.C. ES76SAVILLE, D.A.

The Electrophoresis of Small Particles andFluid Globules in Weak Electrolytes. Forpublication in Journal of Colloid InterfaceScience, Potsdam, NY.

BAYGENTS, J.C. ES76SAVILLE, D.A.

Electrophoresis of Drops and Bubbles. Forpublication in Journal of Chemical Society(London) Faraday Transaction, Cambridge,England.

BAYLESS, E.O. EH42Variable Polarity Plasma Arc Welding. Forpresentation at Technology 2000,Washington, DC, November 27, 1990.

BAYUZICK, R.J.HOFMEISTER, W.H.ROBINSON, M.B.

ES75

Applications of Containerless Processing inthe Studies of Metals and Alloys. Forpresentation at the IKI/AIAA MicrogravityScience Symposium, Moscow, USSR, May1991.

BEARDEN.D.B. EB12LOLLAR, L.F.

Modeling a Constant Power Load for Nickel -Hydrogen Battery Testing Using SPICE. Forpublication in 1990 IECEC Proceedings,Reno, NV, August 1990.

BECHTEL, T.D. EP63TYLER, T.R.

Automated Fluid Interface System. Forpresentation at the JANNAF PropulsionConference, Anaheim, CA, October 3-5,1990.

BENJAMIN, T.G. ED32McCONNAUGHEY, P.K.

Navier-Stokes Analysis of a Liquid RocketEngine Disk Cavity. For presentation at theAIAA/ASME/SAE 27th Joint PropulsionConference and Exhibit, Sacramento, CA,June 24-27,1991.

BERTERO, G.A. ES75HOFMEISTER, W.H.ROBINSON, M.B.BAYUZICK, R.J.

Containerless Processing and RapidSolidification of Nb-Si Alloys of Hyper-Eutectic Composition. For publication inMetallurgical Transactions A, Warrendale,PA.

BILBRO, J.W. EB23JAYROE, R.BAKER, W.

Status of Laser Atmospheric Wind Sounder(LAWS). For presentation at the 6th TopicalMeeting on Coherent Laser Radar, OpticalSociety of America, Snowmass, CO, July 8-12,1991.

BOARDSEN, S.A. ES53GALLAGHER, D.L.GURNETT, D.A.

Reconstruction of Magnetosonic Mode k-Space Spectral Density From ObservedEquatorial Waves. For presentation at the1991 Spring Meeting of the American

29

Page 35: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Geophysical Union, Baltimore, MD, May 28-June 1,1991.

BOOK, M.L. EB24DABNEY, R.HOWARD, R.

Automated Rendezvous and Docking VideoSensor. For presentation at the SpaceOperations, Applications, and ResearchSymposium, Houston, TX, July 9-11,1991.

BRAINERD, J.J. ES65X-Ray Suppression in Gamma-Ray BurstsThrough Resonant Compton Scattering. Forpublication in Proceedings of the Los AlamosGamma-Ray Burst Workshop, Cambridge,MA.

BRAINERD, J.J. ES65MESZAROS, P.

Dynamic Effects on Cyclotron Scattering inPulsar Accretion Columns. For publication inthe Astrophysical Journal, Chicago, IL.

BRAINERD, J.J. ES65The Inability of the Resonant ComptonUpscattering Model of Gamma-Ray Burststo Produce a Third Cyclotron Harmonic. Forpublication in Astrophysical Journal Letters,Cambridge, MA.

BRAINERD, J.J. ES65Multiple Resonant Scattering in the ComptonUpscatter Model of Gamma-Ray Bursts. Forpublication in Astrophysical Journal, Chicago,IL.

BREWER, J.C. EB12Hubble Space Telescope Ground-BasedBattery/Cell Testing at MSFC. Forpresentation at the Aerospace Space PowerWorkshop, El Segundo, CA, April 16-18,1991.

BROWN, D.G. ES53WILSON, G.R.HORWITZ, J.L.GALLAGHER, D:L.

Self-Consistent Production of Ion Conies onReturn Current Region Auroral Field Lines:A Time-Dependent, Semikinetic Model. Forpublication in GRL, Washington, DC.

BROWN, N.S. PD24Lunar Transportation System Options. Forpresentation at AAS/AIAA AstrodynamicsConference, Durango, CO, August 19-22,1991.

BUECHLER, D.E. (USRA)GOODMAN, S.J. ES44

Radar Characteristics of Lightning ProducingStorms in Florida. For presentation at the25th International Conference on RadarMeteorology, Paris, France, June 24-28,1991.

BUKKAPATNAM, S. ED63BATTISTA, B.MAJUMDAR, A.K. (Sverdrup)PIERCE, F.E.PATTERSON, W.C.

Boiling Heat Transfer Analysis During Lossof Coolant in Material Processing Furnacefor Spacelab. For presentation at the 7thInternational Conference on NumericalMethods for Thermal Problems, Stanford,CA, July 8-12,1991.

BUKLEY, A.P ED12A Study of D-Characteristic Equations forTime-Varying Linear Systems UsingCoordinate Transformations. Forpresentation at the Southeastern Symposiumon System Theory, Columbia, SC, March 10-12, 1991.

BUKLEY, A.P. ED12JONES, V.L.PATTERSON, A.F. ED12

NASA/MSFC Large Space StructuresGround Test Facility. For presentation at theAIAA Navigation, Guidance, and ControlConference, New Orleans, LA, August 12-14, 1991.

BURDINE, R.V. AB35BUSHMAN, D.M.

Instrumentation and Calibration Issues forSpace Station Freedom and Future SpaceProjects. For presentation at theAIAA/SOLE 4th Space LogisticsSymposium, Cocoa Beach, FL, November 4-6,1991.

30

Page 36: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

BURNS, D.H. EH43McKECHNIE, T.N.LIAW, Y.

Near Net Shape Fabrication of StructuralRocket Engine Components UtilizingVacuum Plasma Spray. For presentation atthe ASM National Thermal SprayConference, Pittsburg, PA, May 6-10, 1991.

BURNS, R.E. EL58Flight Mechanics Expert Systems. Forpresentation at the AIAA Computing inAerospace Conference, Baltimore, MD,October 22-24, 1991.

BUSH.J.R..JR. EB12LAMER, J.R., JR.

Prelaunch Self Discharge and ChargeAcceptance Characteristics of the HubbleSpace Telescope Nickel Hydrogen Batteries.For presentation at the IECEC andpublication in the Proceedings, Boston, MA,August 4-9, 1991.

CACIOPPO, E. ES76PUSEY, M.L.

The Solubility of the Tetragonal Form of HenEgg White Lysozyme From pH4.0 to 5.4.For publication in The Journal of BiologicalChemistry, Baltimore, MD.

CAMPBELL, J.W. ES52DAVIS, J.M.EMSLIE, A.G.

Imaging the Sun In Hard X-Rays: Spatialand Rotating Modulation Collimators. Forpresentation at the SPIE 36th AnnualInternational Symposium, San Diego, CA,July 21-26, 1991.

CAMPBELL, J.W. ES52DAVIS, J.M.EMSLIE, A.G.

Results From the MSFC Solar Hard X-RayImaging Fourier Telescope NumericalModels. For presentation at the AAS-SolarPhysics Division and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

CANFIELD, A. ThiokolARMOUR, W. AerojetCLINTON, R.G., JR. EH34

Development of Improved AblativeMaterials for ASRM. For presentation at the

AIAA 27th Joint Propulsion Conference,Sacramento, CA, June 24, 1991.

CARDELINO, B. ES74MOORE, C.

Static Second-Order Polarizabilities ofDisubstituted Fused Aromatic Compounds.For presentation at the American ChemicalSociety Southeast-Southwest RegionalMeeting, New Orleans, LA, December 5-7,1990.

CARLSON, G.S. ES43JEDLOVEC, G.J.SUGGS, R.

Remote Sensing of Ozone Variability Usingan Airborne Scanning Infrared Spectrometer.For presentation at the 5th Topical Meetingof Optical Remote Sensing, Williamsburg,VA, November 18-21, 1991.

CARPENTER, D. ES53GILES, B.CHAPPELL, C.DECREAU, P.M.E.CANU, P.ANDERSON, R.CORCUFF, Y.SMITH, A.

A Satellite/Ground Study of Thermal PlasmaStructure and Dynamics in the Dusk BulgeSector of the Magnetosphere. Forpresentation at the 1991 Fall MeetingAmerical Geophysical Union, San Francisco,CA, December 9-13, 1991.

CARPENTER, D.L. ES53SMITH, A.J.GILES, B.L.CHAPPELL, C.R.DECREAU, P.M.E.

A Sunward Taillike Extension of theDuskside Plasmasphere, Scanned byWhistler Ground Stations. For presentationat the 20th General Assembly InternationalUnion of Geodesy and Geophysics, Vienna,Austria, August 11-24, 1991.

CARPENTER, D.L.SMITH, A.J.GILES, B.L.CHAPPELL, C.R.DECREAU, P.M.E.

ES53

31

Page 37: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

A Case Study of Plasma Structure in theDusk Sector Associated With EnhancedMagnetospheric Convection. Forpresentation at the 1990 Fall AGU Meeting,San Francisco, CA, December 3-7, 1990.

CARPENTER, D.L. ES53SMITH, A.L.GILES, B.L.CHAPPELL, C.R.DECREAU, P.M.E.

A Case Study of Plasma Structure in theDusk Sector Associated With EnhancedMagnetospheric Convection. For publicationin Journal of Geophysical Research,Washington, DC.

CARREMGTON, C.K. PD12DAVIS, E.G.

The Application of Linear Actuators forTelescope Pointing Control. For presentationat the 1991 AAS/AIAA AstrodynamicsConference, Durango, CO, August 19-22,1991.

CARRUTH, M.R., JR. EH12VAUGHN, J.A.BECHTEL, R.T.

Electrical Breakdown of Space StationFreedom Surfaces. For presentation at the26th Annual Intersociety Energy ConversionEngineering Conference, Boston, MA,August 4-9, 1991.

CARTER, D. ES76etal.

Modeling Antibody Combining Sites: AMethod for Prediction of the Entire VariableDomain Structure. For publication in Science,Washington, DC.

CARTER, D.C. ES76HE, X-M.TWIGG, P.D.CASALE, E.

Progress on the Structure of Human SerumAlbumin. For presentation at the PittsburghDiffraction Conference, Huntsville, AL,October 20-November 2,1990.

CARTER, D.C.HECHT, D.WITHEROW, W.K.

ES76

NOMAD I: An Imaging Phosphor Detectorfor Application in X-Ray Crystallography,Medical Radiography, and MolecularBiology. For presentation at the PittsburghDiffraction Conference, Huntsville, AL,October 30-November 2, 1990.

CARTER, D.L. ED62HOLDER, D.W.HAYASE, J.K.SHAW, R.G.ALEXANDRE, K. Boeing

Preliminary ECLSS Waste Water Model.For presentation at the 20th InternationalConference on Environmental Systems, SanFrancisco, CA, July 15-18, 1991.

CHOU, L.C. ED31LIAW, G.S.MO, J.D.

Low Thrust Viscous Nozzle Flow FieldPrediction. For presentation at the 27th JointPropulsion Conference and Exhibition,Sacramento, CA, June 24-26, 1991.

CHOU.S-H. ES42MILLER, T.L.

Symmetric Instability in a Growing BaroclinicWave. For presentation at the EighthConference on Atmospheric and OceanicWaves and Stability, Denver, CO, October14-18,1991.

CHOW, AS. EP54Modeling Flow at the Nozzle of a SolidRocket Motor. For presentation at the JointPropulsion Conference, Sacramento, CA,June 24-27,1991.

CHOW, A.S. EP54Adaptive Grid Generation for NumericalModeling Rocket Nozzle Flow. Forpresentation at the IBM Large ScaleAnalysis and Modeling Conference, ParkCity, UT, April 24-26,1991.

CHRISTIAN, H.J. ES43Lightning Observations From Space. Forpresentation at the Conference onAtmospheric Electricity, Alberta, Canada,October 22-26,1990.

32

Page 38: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

CHUBB, S. EO33BRYANT, B. .RAY, J.

Advanced X-Ray Astrophysics Facility(AXAF) Ground Systems Support. Forpresentation at the AIAA 29th AerospaceScience Meeting and Exhibit, Reno, NV,January?, 1991.

CHUBB, W.B. EL01In-Flight Experience and Lessons Learnedin the Attitude Control of a Large SpaceStructure, The Skylab Story. Forpresentation at the International Federationof Automatic Control Workshop, Huntsville,AL, April 2-4,1991.

CIUCCI, A. ED33JENKINS, R.M.FOSTER, W.A.

Numerical Analysis of Ignition Transients inSolid Rocket Motors. For presentation at theAIAA/SAE/ASME/ASEE 27th JointPropulsion Conference, Sacramento, CA,June 24-27, 1991.

CIUCCI, A. ED33FOSTER, W.A.JENKINS, R.

Experimental Investigation of the Flow Fieldin the Head-End Star Slot Section of a SolidRocket Motor. For presentation at theAIAA/SAE/ASME/ASEE 27th JointPropulsion Conference, Sacramento, CA,June 24-27,1991.

CLAYTON, J.L. ED64COLBERT, R.F.GHAFFARIAN, B.MAJUMDAR, A.K.

Prediction of the RSRM Field Joint ThermalEnvironment and Correlation With TestData. For presentation at the AIAA/ASME/SAE/ASEE 27th Joint Propulsion Confer-ence, Sacramento, CA, June 24-27, 1991.

CLEARY, D.D. ES51BOSSERMAN, J.L.TORR. M.R.

Analysis of Middle Ultraviolet DayglowSpectra From the Spacelab 1 ShuttleMission. For publication in Journal ofGeophysical Research, Washington, DC.

COFFEY, V.N. ES53The Effect of Induced Charges on LowEnergy Particle Trajectories NearConducting and Semiconducting Surfaces.For publication in Review of ScientificInstruments, New York, NY.

COLE, H. ED62HABERCOM, M.CRENSHAW, M.JOHNSON, S.MANUEL, S.MARTINDALE, B.WHITMAN, G.TRAWEEK, M.

Characterization of Organic Contaminants inSpace Station Recycled Water. Forpresentation at the SAE IntersocietyConference on Environmental Systems, SanFrancisco, CA, July 15-18,1991.

COMFORT, R.H. ES53HORWITZ, J.L.CRAVEN, P.D.CHAPPELL, C.R.

Characteristic Refilling Rates in thePlasmatrough From Observations by DE-I/RIMS. For presentation at the 20thGeneral Assembly of the International Unionof Geodesy and Geophysics, Vienna,Austria, August 11-24, 1991.

COMFORT, R.H. ES53CRAVEN, P.D.GALLAGHER, D.L.CHAPPELL, C.R.WEST, R.L.

Survey of Thermal O+ TemperaturesObserved In and Near the Plasmasphere byDE-1/RIMS. For presentation at the 20thGeneral Assembly of the International Unionof Geodesy and Geophysics, Vienna,Austria, August 11-24, 1991.

COOPER, A.E. EB22Preliminary Analysis of SSME PlumeEmissions. For presentation at theConference on Health Monitoring for SpacePropulsion Systems, Cincinnati, OH,November 14-15,1990.

COSTES, N.C.LAYMON, C.A.MACARI, E.J.

ES42

33

Page 39: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Small-Scale Field Experiment of LandSurface-Atmosphere Interactions With EOSImplications. For presentation at SPACE 92,3rd International Conference on Engineering,Construction, and Operations in Space,Denver, CO, May 31-June 4, 1992.

COSTES, N.C. ES42MACARI, EJ.MCDONNELL, j.j.

Experimental Techniques for AssessingVegetation-Induced Moisture Flux. Forpresentation at the AGU Fall Meeting, SanFrancisco, CA, December 3-7, 1990.

COWAN, J.R. EP64Design of High Power ElectromechanicalActuator for Thrust Vector Control. Forpresentation at the AIAA/SAE/ASME 27thJoint Propulsion Conference, Sacramento,CA, June 24-26,1991.

CRAVEN, P.D. ES53COMFORT, R.H.RICHARDS, P.G.

A Study of Plasmaspheric N+. Forpresentation at the 1991 Spring MeetingAmerican Geophysical Union, Baltimore,MD, May 28-June 1,1991.

CRONISE, R.J. ES76NOEVER, D.A.

Gravity Effects on Three-DimensionalFroths. For presentation at the Fifth AnnualAlabama Materials Research Conference,Birmingham, AL, September 25-26,1991.

CUMMINGS, R.O. ED63Passively Cooled Infrared TelescopeThermal Math Model Parametric Study. Forpresentation at the Workshop on the NextGeneration Infrared Space Observatory,Edinburgh, Scotland, May 22-24, 1991.

CURRERI, P.A. ES75The Effectiveness of Coriolis Dampening ofConvection During Aircraft High-G Arcs.For publication in Journal of Crystal Growth,North-Holland, Amsterdam.

DAVIDSON, M.TRAWEEK, M.SLIVON, L.SHELDON, L.

IONED62

BattelleResearch Triangle

Space Station Freedom Water RecoveryTest Total Organic Carbon Accountability.For presentation at the 21st IntersocietyConference on Environmental Systems, SanFrancisco, CA, July 15-18,1991.

DAVIS, H.W. ED12BUKLEY, A.P.

Structural Control Sensors for the CASESGTF. For presentation at the ADPA/AIAA/ASME/SPIE Conference on Active Materialsand Adaptive Structures, Alexandria, VA,November 5-7,1991.

DeFOREST, C.E. ES52HOOVER, R.B.et al.

Performance of the Multispectral SolarTelescope Array V: Temperature DiagnosticResponse to the Optically Thin SolarPlasma. For publication in OpticalEngineering, Bellingham, WA.

DELCOURT, D.C. ES53MOORE, T.E.

Precipitation of Ions Induced by MagnetotailCollapse. For publication in Journal ofGeophysical Research, Washington, DC.

DELCOURT, D.C. ES53SAUVAUD, J.A.MOORE, T.E.

Gyro-Phase Effects Near the Storm-TimeBoundary of Energetic Plasma. Forpublication in Geophysical Research Letters,Washington, DC.

DeMAR, P. ESDIPORTER, L.

The Science DECnet Internet and Phase V.For publication in Digital News, Boston,MA.

DENNIS, H. EP62HUTT.J.NESMAN, T.

Stability Testing of a Modified Space ShuttleMain Engine. For presentation at theAIAA/SAE/ASME/ASEE 27th JointPropulsion Conference and Exhibit,Sacramento, CA, June 24-26, 1991.

34

Page 40: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

DEWBERRY, B.S. EB42The ECLSS Advanced Automation Project.For presentation at The Space StationEvolution Symposium, Houston, TX, August6-8,1991.

DEXTER, C.E. EP62ALS LOX/H2 Subscale Coaxial InjectorTesting. For presentation at the AIAA/SAE/ASME/ASEE 27th Joint PropulsionConference, Sacramento, CA, June 24-27,1991.

DOLLMAN, T. EB44WEBSTER, K.

Monitoring and Analysis of Data FromComplex Systems. For presentation atTechnology 2000, Washington, DC,November 27,1990.

DOWDY, J.F., JR. ES52Observational Evidence for EUV LoopsWithin the Supergranular Network. Forpublication in The Astrophysical Journal,Cambridge, MA.

DOWDY, J.F., JR. ES52Observational Evidence for EUV LoopsWithin the Network. For presentation at theAAS-Solar Physics Division and MAX '91Meeting, Huntsville, AL, April 9-12, 1991.

DRISCOLL, K.T. ES43BLAKESLEE, R.J.BAGINSKI, M.E.

Time-Averaged Electric Currents in theVicinity of Isolated Thunderstorms. Forpublication in Journal of GeophysicalResearch, Washington, DC.

DRISKILL, T. ED73Free-Free and Fixed Base Modal SurveyTests of the Space Station Common ModulePrototype. For presentation at theInternational Modal Analysis Conference,San Diego, CA, February 3-6, 1991.

DUGAL-WHITEHEAD, N.R. EB12JOHNSON, Y.

A Study of Fault Injection in MultichannelSpacecraft Power Systems. For presentationat the Intersociety Energy ConversionEngineering Conference (IECEC) 91,Boston, MA, August 4-9, 1991.

EBY, P.B. ES63Cross Section for Production of Low-EnergyElectron-Positron Pairs by RelativisticHeavy Ions. For publication in PhysicalReview A, Ridge, NY.

ELAM, S.K. EP62Subscale Lox/Hydrogen Testing With aModular Chamber and a Swirl CoaxialInjector. For presentation at the AIAA/SAE/ASME 27th Joint Propulsion Conference,Sacramento, CA, June 24-27, 1991.

ELGES.M.R. EB12ASHWORTH, B.R.

Priority Scheme Planning for the RobustSSM/PMAD Testbed. For presentation atthe IECEC Proceedings 1991, Boston, MA,August 3-9,1991.

ELSNER, R.F. ES65O'DELL, S.L.WEISSKOPF, M.C.

Effective Area of the AXAF X-RayTelescope—Dependence Upon DielectricConstants of Coating Materials. Forpublication in Journal of X-Ray Science andTechnology, San Diego, CA.

FARR.R.NESMAN, T.CHASMAN, D.BURNETTE, D.

ED33ED33

RockwellRockwell

Time-Accurate Navier Stokes Computationsof Low Speed Flow Over Cavities: No SlipVersus Blowing Walls. For presentation atthe Fourth International Symposium onComputational Fluid Dynamics, Davis, CA,September 9-12, 1991.

FARR.R.NESMAN, T.CHASMAN, D.BURNETTE, D.

ED33ED33

RockwellRockwell

Time-Accurate Navier Stokes Com-putations: Dynamics of Pressure Oscillationsin the RSRM 80 Seconds After Ignition.For presentation at the Fourth InternationalSymposium on Computational FluidDynamics, Davis, CA, September 9-12,1991.

35

Page 41: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

FARR, R. ED33O'FARRELL, J.M. RockwellBURNETT, D.HOLT, J.FARRIS, T.KRISHNASAMI, Z.

Time-Accurate Fluid Flow Studies UsingRockwell International's USA CFD Code.For presentation at the Technology andBusiness Exposition/Symposium, Huntsville,AL, May 14, 1991.

FAY, J.F. SverdrupSEAFORD, M. ED33

Aerothermodynamic Environment Predic-tions in Support of the Aeroassist FlightExperiment. For presentation at the SeventhAnnual Technical and Business Exhibition(TABES), Huntsville, AL, May 14-15, 1991.

FEARS, S.D. EP62Evaluation of the High Pressure OxidizerTurbopump (HPOTP) Drying Procedures.For presentation at the 27th AIAA/SAE/ASME Joint Propulsion Conference,Sacramento, CA, June 24, 1991.

FICHTL, G.H. ES011991 Atmospheric Environment Highlights.For publication in Aerospace America,Washington, DC.

FIKES, W.K. PD01Requirements and Approaches for the SpaceExploration Initiative Earth to OrbitTransportation. For presentation at theAIAA 1991 International AerospaceEngineering Conference and Show, LosAngeles, CA, February 12-14, 1991.

FINCKENOR, J. ED52Design News Excellence in DesignCompetition—Grip Joint. For publication inDesign News, Newton, MA.

FINCKENOR, M.M. EH15Meteoroid/Space Debris Impacts on A0171Materials. For presentation at the LDEFInvestigators Working Group, Orlando, FL,June 2-8,1991.

FINESCffl, S.HOOVER, R.B.FONTENLA, J.M.etal.

Polarimetry ofAstronomy. For

ES52

EUV Lines in Solarpublication in Optical

Engineering, Bellingham, WA.

ES52FINESCffl, S.HOOVER, R.B.WALKER, A.B.C., JR.

The H-Lyman a Coronagraph/Polarimeter.For presentation at the AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsville,AL, April 9-12,1991.

FINESCffl, S. ES52HOOVER, R.B.WALKER, A.B.C., JR.

H-Lyman a Coronagraph/Polarimetersfor Solar Coronal Magnetic Field Measure-ments. For presentation at SPJJE's Multilayerand Grazing Incidence X-Ray EUV Optics,San Diego, CA, July 21-26,1991.

FISHER, M.F. EP53Analysis of Cryogenic Propellant Behavior inMicrogravity and Low Thrust Environments.For presentation at the AIAA/ASME/SAE27th Joint Propulsion Conference,Sacramento, CA, June 24-27, 1991.

FISHMAN, G.J. ES62The BATSE Experiment on the Gamma-RayObservatory: Capabilities and Early Results.For presentation at the Gamma-RayObservatory Science Workshop, Annapolis,MD, September 23-25, 1991.

FISHMAN, G.J. ES62MEEGAN, C.A.WILSON, R.B.PACIESAS, W.S.PENDLETON, G.N.

The BATSE Experiment on the Gamma RayObservatory: Early Results. Forpresentation at the 178th Meeting of theAmerican Astronomical Society, Seattle,WA, May 26-30, 1991.

36

Page 42: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

HTZJARRALD, D.E. ES42ROBERTSON, F.

Modification of Atmospheric Response byInteractive Surface Hydrology. Forpresentation at the 5th Conference onClimate Variations, Denver, CO, October14-18,1991.

FLOWERS, G.T.RYAN, S.G. ED14

Disk Flexibility Effects on RotordynamicalAnalyses. For presentation at the 36thASME International Gas Turbine andAeroengine Congress and Exposition,Orlando, FL, June 3-6,1991.

FOGLE, F.R. EL56An Improved Exploratory Search Techniquefor Pure Integer Linear ProgrammingProblems. For presentation at the IEEEConference on Systems, Man, andCybernetics, Charlottesville, VA, October13-16,1991.

FOSTER, C.L. ED12TINKER, M.L.NURRE, G.S.TILL, W. A.

The Solar Array-Induced Disturbance of theHubble Space Telescope Pointing System.For presentation at the 61st Shock andVibration Symposium, Pasadena, CA,October 16-18,1990.

FOUNTAIN, J.A. PS05Capabilities for Accommodating ProteinCrystal Growth and X-Ray Diffraction onSpace Station Freedom. For presentation atFuture Directions for the Measurement of X-Ray Intensities From Crystals ofMacromolecules, Gulf Shores, AL, May 17-20, 1991.

FRANCK, C.G. ED25LEE, H.M.

Analysis of a Single Crystal Turbine Bladefor the Space Shuttle Main Engines. Forpresentation at the Fifth InternationalANSYS Conference and Exhibition 1991,Pittsburgh, PA, May 20-24, 1991.

FRAZIER, D. ES74PENN, B.WITHEROW, W.MOORE, C.DOWNEY, J.PALEY, M.CARDELINO, B.

Some Shortfalls in Organic Nonlinear OpticalCrystal Studies. For presentation at SPIE's36th Annual International Symposium, SanDiego, CA, July 21-26, 1991.

FREEMAN, S.E. SverdrupDEATON, A.W. EL58

Mission Analysis of System ArchitectureConcepts for the Space Exploration Initia-tive. For presentation at the Seventh AnnualTechnical and Business Exhibition(TABES), Huntsville, AL, May 14-15, 1991.

GADDIS, S. ED35HUDSON, S.JOHNSON, P.O.

Cold Flow Testing of the Space Shuttle MainEngine Alternate Turbopump Development.For presentation at the 37th ASMEInternational Gas Turbine and AeroengineCongress and Exposition, Cologne,Germany, June 1-4,1992.

GAGLIANO, L.S. EP63MITCHELL, B.K.

Space Station Freedom Seal Development.For presentation at the AIAA 29thAerospace Sciences Meeting and Exhibit,Reno, NV, January 7-10, 1991.

GALLAGHER, D.L. ES53CRAVEN, P.D.COMFORT, R.H.

A Composite Empirical Model ofMagnetospheric Plasma. For presentation atthe 20th General Assembly of theInternational Union of Geodesy andGeophysics, Vienna, Austria, August 16-22,1991.

GALLAGHER, D.L. ES53ASHOUR-ABDALLA, M.

Broadening of Lower-Hybrid Waves byNonlinear Landau Damping. Forpresentation at the 1991 CambridgeWorkshop, Cambridge, MA, June 24-28,1991.

37

Page 43: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

GARCIA, R. ED32Pseudo Three-Dimensional Viscous VoluteAnalysis for the Prediction of Radial Loads.For presentation at the Fourth InternationalSymposium on Computational FluidDynamics, Davis, CA, June 24, 1991.

CARD, M.Y. ED62GEDKE, J.P. McDonnell Douglas

Computer Simulation of the CO2 FireSuppressant Distribution System for SpaceStation Freedom. For presentation at the20th International Conference onEnvironmental Systems, San Francisco, CA,July 15-18, 1991.

GARY, G.A. ES52MUSIELAK, Z.E. UAH

A Regularization Method for theExtrapolation of the Solar Potential MagneticFields. For publication in AstrophysicalJournal, Chicago, IL.

GARY, G.A. ES52A Regularization Method for theExtrapolation of Solar Magnetic Fields. Forpresentation at the Department ofMathematical Sciences at UAH Colloquium,Huntsville, AL, May 10, 1991.

GARY, G.A. ES52MUSIELAK, Z.

A Regularization Method for theExtrapolation of Solar Magnetic Fields. Forpresentation at the AAS-Solar PhysicsDivision and MAX '91 Workshop,Huntsville, AL, April 9-12, 1991.

GENGE, G. EP62Developing Acceptance Limits for MeasuredBearing Wear of the SSME HPOTP. Forpresentation at the 27th AIAA/ASME/SAE/ASEE Joint Propulsion Conference,Sacramento, CA, June 24-27, 1991.

GERMANY, G.A ES51TORR, M.R.TORR, D.G.RICHARDS, P.O.

The Use of VUV Auroral Emissions asDiagnostic Indicators. For publication inJournal of Geophysical Research,Washington, DC.

GERMANY, G.A. ES51TORR, D.G.RICHARDS, P.G.TORR, M.R.

Determination of Ionospheric Conductivitiesfrom VUV Auroral Emissions. Forpublication in Journal of GeophysicalResearch, Washington, DC.

GILL, M.S. EH44Flexible Agricultural Robotics ManipulatorSystem (FARMS). For presentation at theSixth International Conference on CAD/CAM, Robotics, and Factories of the Future,London, U.K., August 19-22,1991.

GILLIES, D.C. ES75LEHOCZKY, S.L.SZOFRAN, F.R.PERRY, G.L.E.SU, C-H.

Interface Demarcation in Bridgman-Stockbarger Crystal Growth of 11-VICompounds. For presentation at the SPIESymposia on Growth and Characterization ofMaterials for Infrared Detectors andNonlinear Optical Switches, Orlando, FL,April 1-5,1991.

GOBBA, W. ES75PATTERSON, J.D.LEHOCZKY, S.L.

Electron Mobility in Mercury Zinc TellurideAlloys. For presentation at the IndianapolisMeeting of the American Physical Society,Indianapolis, IN, March 16-20, 1992.

GOLDBERG, B.E. EP54Hybrid Rocket Technology for Space LaunchVehicles. For publication in AerospaceAmerica, June 1991.

GOODLOE, C.C. EL56GIUDICI, R. J. Sverdrup

Lightning Protection for Shuttle PropulsionElements. For presentation at the 1991International Conference on Lightning andStatic Electricity, Cocoa Beach, FL, April16-19,1991.

38

Page 44: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

GOODMAN, S.J. ES44WRIGHT, P.O.SCHARFEN, G.R.

Development of a Global NighttimeLightning Climatology Using DMSPSatellites. For presentation at the AGU FallMeeting, San Francisco, CA, December 9-13,1991.

GOODMAN, S.J.. ES44BUECHLER, D.E.WRIGHT, P.D.

Lightning-Rainfall Relationships. Forpresentation at the Third Conference onModeling of Rainfall Fields: Hydrologic andMeteorological Aspects, College Station,TX, February 27-March 1, 1991.

GOODMAN, S.J. ES44KNUPP, K.R.

Tornadogenesis via Squall Line andSupercell Interaction Revisited: The 15November 1989 Huntsville Tornado. Forpresentation at the Tornado Symposium III,Norman, OK, April 2-5, 1991.

GOODMAN, S.J. ES44Sensor Fusion Techniques for PredictingThunderstorm Evolution Using Lightning andRadar Networks. For presentation at the25th Conference on Radar Meteorology,Paris, France, June 24-28, 1991.

GOODRICK, T.F. PD33Methodology and Critical PerformanceCharacteristics of Aerobrake Maneuvers forEarth Return. For presentation at the 42ndIAF Congress, Montreal, Canada, October5-11,1991.

GRANT, R. BoeingHOPSON, G. KA01AARON, J.

Space Station Freedom Pressurized ElementInterior Design Process. For presentation atthe 41st International AstronauticalCongress, Dresden, Germany, October 6-13,1990.

GREGORY, J.C.LEGER, L.J.KOONTZ, S.C.VISENTINE, J.PETERS, P.N.

ES63

Effects of Long Term Exposure of PolyimideFilms to the Space Environment. Forpublication in AIAA Journal of Spacecraft andRockets, Washington, DC.

GREGORY, J.C. ES63PETERS, P.N.

Measurement of the Passive AttitudeControl Performance of a RecoveredSpacecraft. For publication in AIAA Journalof Guidance Control and Dynamics,Washington, DC.

GREGORY, J. EB42DEWBERRY, B.LANFEAR, T.McKINNEY, K.GUILLEBEAU, M.TROY, J.

Development of a Pilot Project Following theSpiral Model of Software Development. Forpresentation at The Strategic SoftwareSystems Conference, Huntsville, AL, March10-11,1992.

GRINER, C.S. EO01Space Station Freedom Payload Operationsin the 21st Century. For presentation at the42nd International Astronautical Congress,Montreal, Canada, October 7-11, 1991.

GROSS, K.W. EP55CFD Code Survey for Thrust ChamberApplication. For presentation at theJANNAF Combustion Meeting, Cheyenne,WY, November 5-9,1990.

GUFFIN, T. EO43OLSEN, C.ONKEN, J.

A Practical Approach to Astronomy MissionReplanning. For presentation at the AIAASpace Programs and TechnologiesConference, Huntsville, AL, March 24-27,1992.

GUILLORY, A.R. ES43A Physical Split Window Technique for theRetrieval of Precipitable Water FromSatellite Measurements. For presentation atthe Sixth Conference on SatelliteMeteorology and Oceanography, Atlanta,GA, January 5-10, 1992.

39

Page 45: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

GUILLORY, A. ES43A Physical Split Window Technique forDeriving Precipitable Water Utilizing VASData. For presentation at the TopicalMeeting on Optical Remote Sensing,Williamsburg, VA, November 18-21, 1991.

HAGYARD, MJ. ES52WEST, E.A.KENNY, E.G.

Magnetic Field Configuration AssociatedWith Gamma-Ray Flares in June 1991. Forpresentation at the Gamma-RayObservatory Science Workshop, Annapolis,MD, September 25, 1991.

HAGYARD, MJ. ES52HEYVAERTS, J.

On the Energy Storage in Solar Flares. Forpublication in Flares 22 WorkshopProceedings, Chantilly, France.

HAGYARD, MJ. ES52GARY, G.A.MOORE, R.L.

The MSFC Solar GRO Guest Investigation.For presentation at AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsville,AL, April 9-12,1991.

HAGYARD, MJ. ES52WEST, E.A.GARY, G.A.SMITH, J.E.

Magnetic Field Changes Associated With aSubflare and Surge. For presentation atAAS-Solar Physics Division and MAX '91Meeting, Huntsville, AL, April 9-12, 1991.

HAMMOND, M. EP64LACKEY,!.MYERS, W.N.

Design of Vacuum Plasma Spray Handler.For presentation at the 26th AerospaceMechanisms Symposium, Greenbelt, MD,May 13-15 1992.

HAMPTON, D. EB23JONES, W.ROTHERMEL, J.

Development and Performance of a DigitalSignal Processing System for CoherentLaser Radar. For presentation at the Sixth

Topical Meeting on Coherent Laser Radar,Snowmass, CO, July 8-12,1991.

HAN, S. EP55BAI, S.D.SCHAFER, C.F.

Ignition Transient Analysis of Solid RocketMotor. For presentation at the AIAA 22ndFluid Dynamics Plasma Division, Waikiki,HI, June 24-26, 1991.

HANSON, J.M. EL58Use of Multiple Lunar Swingby for Departureto Mars. For presentation at the AAS/AIAAAstrodynamics Conference, Durango, CO,August 19-22, 1991.

HARMON, B.A. ES62WILSON, R.B.FINGER, M.H.PACIESAS, W.S.FISHMAN, GJ.MEEGAN, C.A.

Occultation Analysis of BATSE Data-Operational Aspects. For presentation at theGamma-Ray Observatory ScienceWorkshop, Annapolis, MD, September 23-25,1991.

HARMON, B.A. ES62FISHMAN, GJ.PARNELL, T.A.LAIRD, C.E.

Induced Radioactivity in LDEF Components.For presentation at the First LDEF Post-Retrieval Symposium, Orlando, FL, June 2-8,1991.

HARRIS, T.L. PP02DICKERSON, T.D.GERRY, M.D.

Aerobrake Concepts and Schedules for Lunarand Mars Missions. For presentation at the28th Space Congress, Cocoa Beach, FL,April 23-26, 1991.

HARSH, M.BENNER, J.GARABETIAN, A.BURG, R.

EP01RockwellRockwellRockwell

Shuttle-C Auxiliary Propulsion SystemCertification Approach and Low-CostEvolution Concepts. For presentation at the

40

Page 46: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

AIAA Joint Propulsion Conference,Sacramento, CA, June 24-26,1991.

HASTINGS, L.J. EP53HUFFAKER, F.TUCKER, S.

Lunar Mission Scenarios, Transfer VehicleConcepts, and Cryogenic Fluid ManagementNeeds. For presentation at the AIAAConference on Advanced SEI Technologies,Cleveland, OH, September 3-6, 1991.

HATHAWAY, D.H. ES52Spherical Harmonic Analysis of SteadyPhotospheric Flows II. For publication inSolar Physics, Hingham, MA.

HATHAWAY, D.H. ES52RHODES, E.J., JR.etal.

The Supergranulation Spectrum. Forpublication in Proceedings of the"Conference on Challenges to Theories ofthe Structure of Moderate Mass Stars,"Santa Barbara, CA.

HATHAWAY, D.H. ES52RHODES, E.J.KORZENNIK, S.CACCIANI

Rotation Rate of the SupergranulationPattern. For presentation at the AAS-SolarPhysics Division and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

HE, X-M. ES76RUKER, F.CARTER, D.C.

The Structure of a Human MonoclonalAntibody Against GP-41 of HumanImmunodeficiency Virus Type I. Forpublication in Science, Washington, DC.

HE, X-M. ES76CARTER, D.C.CASALE, E.

Structure of a Fab From a HumanMonoclonal Antibody Against GP-41 of theHuman Immunodeficiency Virus Type I(HIV-1) and Antigen Complex. Forpresentation at the Pittsburgh DiffractionConference, Huntsvile, AL, October 30-November 2, 1990.

HE, X-M. ES76CARTER, D.C.TWIGG, P.O.

Progress on the Structure of a Novel FungalLysozyme From Chalaropsis. Forpresentation at the Pittsburgh DiffractionConference, Huntsville, AL, October 30-November 2, 1990.

HEAMAN, J.P. ED35Performance and Calibration Results of theMSFC Cold Flow Turbine Test Facility. Forpresentation at the 75th Semiannual Meetingof the Supersonic Tunnel Association,Austin, TX, April 29-30, 1991.

HEAMAN, J.P. ED35A Directional Probe Calibration Facility. Forpresentation at the 75th Semiannual Meetingof the Supersonic Tunnel Association,Austin, TX, April 29-30,1991.

HEDIGER, L.H. EH13An Assessment of Artifact DiscriminationTechniques for Homogeneous Materials. Forpresentation at the NondestructiveEvaluation for Aerospace Requirements,Huntsville, AL, June 4-6, 1991.

HEDIGER, L. EH13BROWN, R.

A Reliability Assessment for the AdvancedComputed Tomography Inspection System(ACTIS). For presentation at the AmericanSociety for NDE-CT Topical, San Diego, CA,May 28, 1991.

HERREN, B.J. JA84Patent No. 4,919,899 "Crystal GrowthApparatus." For presentation at the CrystalGrowth of Biological Materials Conference,Freiburg, FRG, August 18-24, 1991.

HINMAN, E.M. EB24Robosim, A Simulator for Robotic Systems.For presentation at Technology 2000,Washington, DC, November 27-28, 1990.

HINMAN, E.M. EB24WORKMAN, G.

Characterizing Microgravity Performance of aLaboratory Robot. For presentation at theInternational Robots and Vision Automation

41

Page 47: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Show and Conference, Detroit, MI, October22-24,1991.

HO, C.W. ES53HORWTTZ, J.L.SINGH, N.WILSON, G.R.MOORE, T.E.

Effects of Magnetospheric Electrons on PolarPlasma Outflow: A Semikinetic Model. Forpublication in Journal of GeophysicalResearch, Washington, DC.

HOLDEN, C., JR. EB44SAVAGLIO, C.

Math Model Partitioning in Advanced EngineDesign Simulations. For presentation atADIUS '91 12th Annual Conference,Burlington, VT, June 23-27,1991.

HOODLESS, R.M. HA01MONK, J.C.CIKANEK, H.A., ffl

Advanced Launch System SpaceTransportation Main Engine. Forpresentation at the 42nd InternationalAstronautical Congress, Montreal, Canada,October 5-11,1991.

HOOVER, R.B. ES52etal.

The Multispectral Solar Telescope Array IV:The Soft X-Ray and Extreme UltravioletFilters. For publication in OpticalEngineering, Bellingham, WA.

HOOVER, R.B. ES52etal.

Development of the Water Window ImagingX-Ray Microscope Utilizing NormalIncidence Multilayer Optics. For publicationin Optical Engineering, Bellingham, WA.

HOOVER, R.B. ES52FINESCHI, S.FONTENLA, J.M.etal.

Imaging Polarimeters for Solar EUVAstronomy. For publication in OpticalEngineering, Bellingham, WA.

HOOVER, R.B.BAKER, P.C.etal.

ES52

Water Window Imaging X-Ray Microscopefor Cancer Research. For presentation atTechnology 2000, Washington, DC,November 27-28,1990.

HOOVER, R.B. ES52etal.

Fabrication and Testing of an ImagingMultilayer X-Ray Microscope. Forpresentation at the Multilayer and GrazingIncidence X-Ray EUV Optics, SPIE, SanDiego, CA, July 21-26,1991.

HOOVER, R.B. ES52etal.

Design and Analysis of a Multimirror Soft X-Ray Imaging Microscope. For presentationat SPIE's Multilayer and Grazing IncidenceX-Ray/EUV Optics, San Diego, CA, July 21-26,1991.

HOOVER, R.B. ES52etal.

Development of a Water Window ImagingX-Ray Microscope. For presentation atSPIE's Multilayer and Grazing Incidence X-Ray EUV Optics, San Diego, CA, July 21-26,1991.

HOOVER, R.B. ES52etal.

Solar Observations With the MultispectralSolar Telescope Array. For presentation atSPIE's Multilayer and Grazing Incidence X-Ray EUV Optics, San Diego, CA, July 21-26,1991.

HOOVER, R.B. ES52etal.

Optical Configurations of H-Lyman aCoronagraph/Polarimeter Instruments. Forpresentation at SPIE's Multilayer andGrazing Incidence X-Ray EUV Optics, SanDiego, CA, July 21-26,1991.

HOOVER, R.B. ES52WALKER, A.B.C., JR.LINDBLOM, J.BARBEE, T.W., JR.

The Multispectral Solar Telescope Array.For presentation at AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsville,AL, April 9-12,1991.

42

Page 48: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

HOOVER, R.B. ES52WALKER, A.B.C., JR.LINDBLOM, J.BARBEE, T.W., JR.

The Multispectral Solar Telescope Array.For presentation at AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsville,AL, April 9-12,1991.

HOPPE, D. EH44BABAI, M.K.

High Pressure Waterjet Cutting andStripping. For presentation at Technology2000, Washington, DC, November 27, 1990.

HOPSON, G.D. KA01Verification of Space Station FreedomElements and Systems. For presentation atthe 42nd IAF Congress, Montreal, Canada,October 5-11,1991.

HORWITZ, J.L. ES53POLLOCK, C.J.MOORE, T.E.PETERSON, W.K.BURCH, J.L.WINNINGHAM, J.D.CARVEN, J.D.FRANK, L.A.PERSOON, A.

On Outflowing O+ Beams in the Polar CapRegions. For publication in Journal ofGeophysical Research, Washington, DC.

HOWARD, S. ES62The GRO/BATSE Data Analysis System.For presentation at the Astronomical DataAnalysis Software and System AnnualConference, Tucson, AZ, November 6-8,1991.

HOWARD, S. ES62Gamma-Ray Observatory/BATSE Status.For presentation at the 22nd DDA Meetingof AAS, Key Biscayne, FL, May 16-18,1991.

HUBER, W.G. PA01SUMRALL, J.P. PT41

Establishing the Infrastructure: AnIntegrated Space Transportation System.For presentation at the Mars Exploration—Past, Present, and Future (AIAA Meeting),Williamsburg, VA, July 16-19,1991.

HUBER, W.G. PA01SUMRALL, J.P.

Space Transportation Options for the SpaceExploration Initiative. For presentation atthe 42nd IAF Congress, Montreal, Canada,October 5-11,1991.

HUDSON, S. ED35BOYNTON, J.L.TABIBZADEH, R.

Investigation of the Effect of Rotor BladeRoughness on Turbine Performance. Forpresentation at the 37th ASME InternationalGas Turbine and Aeroengine Congress andExposition, Cologne, Germany, June 1-4,1992.

HUDSON, S. ED35GADDIS, S.TRAN, K.CHAN, D.CHEN, S.

Analysis of the Space Shuttle HPFTPTurbine and Comparison With Air Test Data.For presentation at the 37th ASMEInternational Gas Turbine and AeroengineCongress and Exposition, Cologne,Germany, June 1-4,1992.

HUDSON, S.T. ED35GADDIS, S.W.JOHNSON, P.O.BOYNTON, J.L.

Cold Flow Testing of the Space Shuttle MainEngine High Pressure Fuel Turbine Model.For presentation at the AIAA/SAE/ASME/ASEE 27th Joint PropulsionConference, Sacramento, CA, June 24-27,1991.

HUETER, U. PT21BRADY, H.EVANS, R.

NASA's Heavy-Lift Cargo Launch VehicleNeeds and Options for the Post-2000 Period,For presentation at the 28th SpaceCongress, Cocoa Beach, FL, April 23-26,1991.

HUMPHRIES, W.R. ED61Spacecraft Thermal and Manned DesignEnvironments. For presentation at theIDEES Conference, Houston, TX, November

- 12-15,1991.

43

Page 49: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

HUMPHRIES, W.R. ED61BAGDIGIAN, R.M.

Water Purification and Standards. Forpresentation at the Technology 2000Conference, Washington, DC, November 27,1990.

HUMPHRIES, W.R. ED61A Survey of Spacecraft Thermal DesignSolutions. For presentation at the FourthEuropean Symposium for Space StationEnvironmental Control Systems, Florence,Italy, October 21-25,1991.

HUMPHRIES, W.R. ED61PERRY, J.L.

Monitoring and Control of Atmosphere in aClosed Environment. For presentation at theTechnology 2000 Conference, Washington,DC, November 27, 1990.

HUNG, RJ. ES42LEE, C.C.LESLIE, F.

Slosh Wave Excitation in a Partially FilledRotating Tank Due to Gravity-Jitters in aMicrogravity Environment. For publication inActa Astronautica, Paris, France.

HUNG, R.J. ES44LEE, C.C.JOHNSON, D.L.CHEN, AJ.

Remote Sensing Density PerturbationsInduced by Subtropical Rainfalls forSpacecraft Environment Study. Forpresentation at the Seventh Annual TABES91, Huntsville, AL, May 14-15, 1991.

HUNG, RJ. ES44LEE, C.C.JOHNSON, D.L.CHEN, AJ.

Remote Sensing of Mesospheric andThermospheric Density PerturbationsInduced by Subtropical Heavy Rainfalls forSpacecraft Environment Study. Forpublication in Acta Astronautica Volume 23,1991.

INGUVA, R.JOHNSON, S.C.JONES, W.D.BILBRO, J.W.

EB23

Maximum Entropy and Bayesian Methodsfor Processing LIDAR/LAWS Data. Forpresentation at the Sixth Topical Meeting onCoherent Laser Radar, Snowmass, CO, July8-12,1991.

IYONO, A. ES62TAKAHASHI, Y.GREGORY, J.C.CHRISTL, M.J.DERRICKSON, J.H.FOUNTAIN, W.F.PARNELL, T.A.etal.

Rapidity and Transverse MomentumDistributions in 6.4 TeV S + Pb InteractionsFrom Cern EMU05 Experiments. Forpresentation at the 22nd InternationalCosmic Ray Conference, Dublin, Ireland,August 11-23, 1991.

JAKSTAS.L.M. EB12RIEDESEL, J.D.MYERS, CJ.

User Interface Design Principles for theSSM/PMAD Automated Power System. Forpresentation at the IECEC Proceedings1991, Boston, MA, August 3-9, 1991.

JEDLOVEC, GJ. ES43ATKINSON, RJ.

Variability of Geophysical Parameters fromAircraft Radiance Measurements (for FIFE).For publication in Journal of GeophysicalResearch, Washington, DC.

JEDLOVEC, GJ. ES43JAMES, M.W.SMITH, M.ATKINSON, R.

A PC-Based Multispectral Scanner DataEvaluation Workstation: Application toDaedalus Scanners. For presentation at theFourth Airborne Geoscience Workshop,LaJolla, CA, January 29-February 1, 1991.

JOHNSON-COLE, H. EB23Variable Sensitivity Moire Interferometry.For presentation at the Society forExperimental Mechanics Spring Conference,Milwaukee, WI, June 10-13,1991.

44

Page 50: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

JOHNSON, C.L. PS02Space Exploration Initiative Lunar-BasedSpace Physics Missions. For presentation atthe 28th Space Congress, Cocoa Beach, FL,April 23-26,1991.

JOHNSON, C.L. PS02DIETZ, K.L.

Effects of the Lunar Environment on OpticalTelescopes and Instruments. For presenta-tion at the Space Astronomical Telescopesand Instruments, sponsored by SPIE,Orlando, FL, April 1-5, 1991.

JOHNSON, D.L. ES44Overview of the X-30 Natural Environment.For presentation at the 10th NationalAerospace Plane Symposium, Monterey,CA, April 23-26,1991.

JOHNSON, S.C. EB23Shuttle Wind Profiler. For presentation atthe Sixth Topical Meeting on Coherent LaserRadar, Snowmass, CO, July 8-12, 1991.

JOLLY, C.D. ED62SCHUSSEL, L.CARTER, D.L.

Advanced Development of ImmobilizedEnzyme Reactors. For presentation at the20th International Conference onEnvironmental Systems, San Francisco, CA,July 15-18, 1991.

JONES, C.S. EH42BREWER, W.V.

Mechanisms for Robotic Assembly ofWelded Truss Structures in Space. Forpresentation at the 26th AerospaceMechanisms Symposium, GSFC, Greenbelt,MD, May 13-15, 1992.

JONES, C.S. EH42In-Space Welding for Assembly,Construction, and Repair. For presentationat the In-Space Assembly/Servicing FacilityWorkshop, LaRC, Hampton, VA, July 25,1991.

JONES, C.S., III EH42Robotics in Space-Age Manufacturing. Forpresentation at Technology 2000,Washington, DC, November 27, 1990.

JONES, C.S., III EH42Robotics in Aerospace Manufacturing. Forpresentation at the IEEE Society Chapter,Huntsville, AL, January 18,1991.

JONES, L.W. EP53FISHER, M.F.McCOOL, A.A.MCCARTY, J.P.

Propulsion at the Marshall Space FlightCenter: A Brief History. For presentation atthe AIAA/ASME/SAE 27th Joint PropulsionConference, Sacramento, CA, June 24-27,1991.

JOY, M. ES65WEISSKOPF, M.C.

Development of Hard X-Ray Optics. Forpresentation at SPIE's 1991 InternationalSymposium, San Diego, CA, July 21-26,1991.

KAARET, P. ES65WEISSKOPF, M.ELSNER, R.RAMSEY, B.etal.

The Stellar X-Ray Polarimeter for theSpectrum-X-Gamma Mission. Forpublication in Proceedings IAU No. 123,Boston, MA.

KARR, L.J. ES76DONNELLY, D.L.KOSLOWSKY, A.HARRIS, J.M.

Comparisons of Reagents for ImmunoaffinityPartition. For presentation at Advances inSeparations in Biochemistry, Cell Biology,and Biotechnology, New Orleans, LA, June2-7,1991.

KAVAYA, M.J. EB23FREHLICH, R.G.

Single Particle Mode Coherent JJdarMeasurements of Aerosol Backscatter: ErrorSources and Calibration. For presentation atthe Sixth Topical Meeting on Coherent LaserRadar, Optical Society of America,Snowmass, CO, July 8-12, 1991.

KAVAYA, M.J.SUNI, P.J.M.

EB23

45

Page 51: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Analytic Solution for the Location andVolume of CW Coherent Lidar AtmosphericMeasurements. For presentation at theSixth Topical Meeting on Coherent LaserRadar, Optical Society of America,Snowmass, CO, July 8-12, 1991.

KIEFLING, L.A. ED22MULLER, G.SAXON, J.VIALL, W.PRICKETT, T.FARRIS, T.KRISHNASAMI, Z.

Modeling Structural Dynamic Behavior ofSSME Components. For presentation at theTechnology and Business Exposition/Symposium, Huntsville, AL, May 14, 1991.

KING, D.T. ES62DERRICKSON, J.H.EBY, P.B.FOUNTAIN, W.F.GREGORY, J.C.MOON, K.H.OGATA, T.PARNELL, T.A.et al.

Energy Dependence for Direct PairProduction Using Relativistic Oxygen Ions.For presentation at the 22nd InternationalCosmic Ray Conference, Dublin, Ireland,August 11-23, 1991.

KING, M.S. EB14A Map-to-Data Highway ImplementationUsing MMS. For presentation at IEEESoutheastcon '91, Williamsburg, VA, April7-10, 1991.

KIRKINDALL, A.S. JA83Space Station Furnace Facility—A Multi-purpose, High Temperature MicrogravityResearch Facility. For presentation at the42nd International Astronautical Congress,Montreal, Canada, October 5-11, 1991.

KOCZOR, RJ. ES41NASA's Geostationary Earth Observatory(GEO). For presentation at the SPIE 1991International Symposium on Optical AppliedScience and Engineering, San Diego, CA,July 21-26, 1991.

KOSHAK, W. ES43A Numerical Model for Lightning RadiativeTransfer. For presentation at the 1991American Geophysical Union Fall Meeting,San Francisco, CA, December 9-13, 1991.

KUMAR, G.N. SverdrupGRIFFITH, D.O.RUF, J. ED32

SSME Engine 0209 Hot Gas Leak FlowCFD Analysis. For presentation at theAIAA 30th Aerospace Sciences Meeting,Reno, NV, January 6-9,1992.

KUSUNOSE, M. ES65MINESHIGE, S.

Pair Density Transitions in Accretion DiskCoronae. For publication in TheAstrophysical Journal, Chicago, IL.

KUSUNOSE, M. ES65MINESHIGE, S.

A Limit-Cycle Behavior of Pair Density inAccretion-Disk Coronae. For presentation atthe 28th Yamada Conference on Frontiers ofX-Ray Astronomy, Nagoya, Japan, April 8-12,1991.

KYNARD, M.H. EE23DILL, G.A.

SSME Testing Technology at Stennis SpaceCenter. For presentation at the 1991Aerospace Atlantic Conference, Society ofAutomotive Engineers, Dayton, OH, April22-26, 1991.

LANIER, G.D. PD34VIZZIER, B.

ESDOTS, An Object Oriented KnowledgedBased System for Space Vehicle ProcessingAnalysis. For presentation at the 1991Summer Computer Simulation Conference,Baltimore, MD, July 22-24, 1991.

LAPENTA, W.M. ES42The Role of SST Distributions in ModulatingPBL Structure and Surface Energy FluxesDuring ERICA: Numerical Simulations. Forpresentation at the Fifth Conference onMesoscale Processes, Atlanta, GA, January5-10,1992.

LAPENTA, W.M.SEAMAN, N.L.

ES42

46

Page 52: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

A Numerical Investigation of East-CoastCyclogenesis During the Cold-Air DammingEvent of 27-28 February 1982, Part II:Importance of Physical Mechanisms. Forpublication in Monthly Weather Review,Boston, MA.

LAPENTA, W.M. ES42PERKEY, D.J.KREITZBERG, C.ROBERTSON, F.

The Role of SST Distributions in ModulatingPBL Structure and Surface Energy FluxesDuring ERICA: Numerical Solutions. Forpresentation at the Ninth Conference onNumerical Weather Prediction, Denver, CO,October 14-18, 1991.

LAWLESS, K.G., III EH42Marshall Automated Weld SystemPresentation. For presentation at theAeromat '91 Conference—ASM, LongBeach, CA, May 20-24, 1991.

LAWSON, L.M. AuburnPEREZ, J.D.MOORE, T.E. ES53CHAPPELL, C.R.

O+ Phase Space Densities From RIMS onDE 1. For presentation at the 1991 FallAGU Meeting, San Francisco, CA,December 9-13, 1991.

LEE.S.C. EB12RATLIFF, M.PETERSON, C. UTSILOLLAR, L.

Amperes: A Real Time Monitoring andDiagnosis KBS for Space Power Systems.For publication in Applied AI: AnInternational Journal, New York, NY, May30, 1991.

LESLIE, F.W. ES42HUNG, R.J.LEE, C.C.

Gravity Probe-B Spacecraft Attitude ControlBased on the Dynamics of Slosh Wave-Induced Fluid Stress Distribution onRotating Dewar Container of CryogenicPropellant. For presentation at the 42ndCongress of the IAF, Montreal, Canada,October 5-11, 1991.

LESLIE, F.W. ES42HUNG, RJ.LEE, C.C.

Longitudinal and Transverse Modes of SloshWave Excitation in Rotating DewarAssociated with Gravity Jitters. Forpresentation at the 42nd Congress of theInternational Astronautical Federation,Montreal, Canada, October 5-11, 1991.

LESLIE, F.W. ES42HUNG, RJ.LEE, C.C.

Spacecraft Dynamical Distribution of FluidStresses Activated by Gravity Jitter InducedSlosh Waves. For publication in Journal ofGuidance, Control, and Dynamics,Washington, DC.

LIN, N. ES53ENGEBRETSON, M.J.REINLEITNER, L.A.OLSON, J.V.GALLAGHER, D.L.CAHILL, L.J.SLAVIN, J.A.PERSOON, A.M.

Field and Thermal Plasma Observations ofULF Pulsations During a MagneticallyDisturbed Interval. For publication in Journalof Geophysical Research, Washington, DC.

LINTON,R.C. EH12REYNOLDS, J.M.

LDEF Experiment A0034: Interim Results.For presentation at the LDEF First Post-Retrieval Symposium, Kissimmee, FL, June2-8,1991.

LIU, C. AuburnPEREZ, J.D.MOORE, T.E. ES53CHAPPELL, C.R.

H+ Phase Space Densities From RIMS onDE 1. For presentation at the 1991 FallMeeting/AGU, San Francisco, CA,December 9-13,1991.

LOLLAR, L.F. EB12Automating a Spacecraft Electrical PowerSystem Using Expert Systems. Forpresentation at JEA/AIE-91, Kauai, HI, June2-5,1991.

47

Page 53: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

LOLLAR.L.F. EB12HALL, O.K.DORESWAMY, R.

The Space Station Module PowerManagement and Distribution AutomationTest Bed. For presentation at theIntersociety Energy Conversion EngineeringConference (IECEC), Boston, MA, August3-9,1991.

LOMAS, J.J. EL58DEATON, A..W. EL58

Autonomous Rendezvous TargetingTechniques for National Launch SystemsApplications. For presentation at theAutomatic Rendezvous and Capture Review,Williamsburg, VA, November 19-21, 1991.

LOONEY, A. EH42Welding Technology Transfer Task for Cope-land Corporation. For presentation at theHuntsville Chapter of American WeldingSociety, Madison, AL, January 24, 1991.

LOWER Y.J.E. EB12MAI,J.

Nickel Hydrogen LEO Cycling at 20-50Percent Depth of Discharge. Forpresentation at the IECEC, Boston, MA,August 4-9, 1991.

LU, H-I. ES42MILLER, T.L.FITZJARRALD, D.

Interannual Variability in a 3-D BaroclinicFlow Model With Periodic Changes ofThermal Forcing. For presentation at theEighth Conference on Atmospheric andOceanic Waves and Stability, Denver, CO,October 14-18, 1991.

LU, H-I. ES42MILLER, T.L.

Wave-Mean Flow Interactions During anAmplitude Vacillation. For presentation atthe Eighth Conference on Atmospheric andOceanic Waves and Stability, Denver, CO,October 14-18,1991.

LYNCH, K.A.ARNOLDY, R.L.POPECKI, M.KINTNER, P.M.CAHILL,L.J.,JR.

ES53

MOORE, T.E.POLLOCK, CJ.

Temporal Evolution of Auroral ElectronDistribution Functions From the ARCS4Sounding Rocket. For presentation at the1991 Spring AGU Meeting, Baltimore, MD,May 28-June 1,1991.

McCARLEY, K.S. EL53BAER-PECKHAM, M.S.

The Integration of Microgravity ScienceExperiments Into Shared or PreviouslyExisting Experiment Facilities. Forpresentation at the AIAA NationalAerospace Sciences Conference, Reno, NV,January?, 1991.

MCCARTY, J.P. EPOIRocket Propulsion for NASA's Earth to OrbitLaunchers. For presentation at the LauncherPropulsion Towards the Year 2010Symposium, Bordeaux, France, June 10-11,1991.

McCONNAUGHEY, H. EPOILYLES, G.M.

Space Transportation Engine Cycle SelectionProcess. For presentation at the AIAA/SAE/ASME/ASEE 27th Joint PropulsionConference, Sacramento, CA, June 24-26,1991.

McGRIFF, C.F. ED62CARTER, D.L.CARRASQUILLO, R.L.OGLE, K.HOLDER, D.W., JR.

ECLSS Regenerative Systems ComparativeTesting and Selection. For presentation atthe 21st Intersociety Conference onEnvironmental Systems, San Francisco, CA,July 15-18,1991.

McINTYRE, S. EP53FADDOUL, J.R.

The NASA Cryogenic Fluid ManagementTechnology Program Plan. For presentationat the AIAA/NASA/OAI AdvancedExploration Initiative Conference, Cleveland,OH, September 4-6, 1991.

McKINNEY, K.SHACKELFORD, K.

GDIEB42

48

Page 54: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

An Approach to Developing User Interfacesfor Advanced Space System. For pre-sentation at the International Space YearConference on Earth and Space ScienceInformation Systems, Pasadena, CA,February 10-13, 1992.

MACHADO, M.E. ES52MOORE, R.L.

Magnetic Energy Storage and Conversion inTransient Solar Activity-Observations. Forpublication in Proceedings of SCOSTEPInternational Solar-Terrestrial PhysicsSymposium, The Netherlands.

MARTINEZ, L.F.McCLURE, J.C.NUNES, A.C., JR. EH42

The Effect of Gas Contamination DuringWelding of Aluminum-Lithium Alloys. Forpresentation at and publication in the 1991ASME Winter Annual Meeting ASMEJournal of Engineering for Industry, Atlanta,GA, December 1-6, 1991.

MILLER, T. ES42Microgravity Experiments and NumericalSimulations of Rotating Convection in aHemispherical Layer. For presentation at theSoutheastern Conference on Theoretical andApplied Mechanics, Nashville, TN, April 12-14, 1992.

MILLER, T.L. ES42REYNOLDS, N.D.

A Laboratory and Numerical Study ofBaroclinic Instability in a Cylindrical AnnulusWith the Temperature Gradient Imposed onthe Lower Surface. For publication in Journalof Fluid Mechanics, Cambridge, UK.

MILLER, T.L. ES42LU, H-I.BUTLER, K.A.

A Fully Nonlinear, Mixed Spectral and FiniteDifference Model for Thermally DrivenRotating Flows. For publication in Journal ofComputational Physics, Duluth, MN.

MILLER, T.L. ES42Comments on "Convection in a Rotating,Laterally Heated Annulus: Transition toLower Symmetry." For publication in

Geophysical and AstrophysicalDynamics, New York, NY.

Fluid

MIN, J. ED25Submodeling Approach for SSME HPOTPHousing Stress Analysis. For presentationat the Fifth International ANSYS Conferenceand Exhibition 1991, Pittsburgh, PA, May•20-24,1991.

MITCHELL, B.K. EP63Internally Replaceable Seals for OuterspaceHabitats. For presentation at the AIAA 29thAerospace Sciences Meeting and Exhibit,Reno, NV, January 7-10,1991.

MITCHELL, R.E. SA61The Advanced Solid Rocket Motor for theSpace Shuttle. For presentation at the 42ndIAF Congress, Montreal, Canada, October5-11,1991.

MOON, K.H. ES62DERRICKSON, J.H.EBY, P.B.FOUNTAIN, W.F.PARNELL, T.A.TAKAHASHI, Y.et al.

Measurements of Direct Electron PairsAlong Oxygen and Sulfur Ion Tracks at 200GeV/n. For presentation at the 22ndInternational Cosmic Ray Conference,Dublin, Ireland, August 11-23, 1991.

MOORE, R.L. ES52Triggering of Eruptive Flares: Distabilizationof the Preflare Magnetic Field. Forpresentation at the IAU Colloquium No. 133on Eruptive Solar Flares, Iguazu, Argentina,August 2-6, 1991.

MOORE, R.L. ES52MUSIELAK, Z.E.SUESS, S.T.AN, C.-H.

Alfven Wave Trapping in Coronal Holes andSubsequent Heating. For presentation at theSolar Wind Seven, Goslar, Germany,September 16-20, 1991.

49

Page 55: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

MOORE, R.L. ES52HAGYARD, MJ.DAVIS, J.M.PORTER, J.G.

The MSFC Vector Magnetograph, EruptiveFlares, and the Solar-A X-Ray Images. Forpresentation at the IAU General AssemblySolar Sessions, Buenos Aires, Argentina,July23-Augustl, 1991.

MOORE, R.L. ES52A Novel Way to Concert Alfven Waves toHeat in Coronal Holes: Reflective Damping.For presentation at the AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsvillle,AL, April 9-12,1991.

MOORE, R.L. ES52HAGYARD, M.J.DAVIS, J.M.PORTER, J.G.

The MSFC Vector Magnetograph, EruptiveFlares, and the Solar-A X-Ray Images. Forpublication in Proceeedings of Solar-AScience Meeting, Tokyo, Japan.

MOORE, R.L. ES52MUSELAK, Z.E.SUESS, S.T.AN, C.-H.

Alfven Wave Trapping, Network Microflaringand Heating in Solar Coronal Holes. Forpublication in The Astrophysical Journal,Chicago, IL.

MOORE, T.E. ES53POLLOCK, C.J.ARNOLDY, R.L.CAHILL, L.J., JR.KINTNER, P.M.

ARCS4 Experiment: Plasma Heating andFlow Observations. For presentation at the1991 Spring Meeting American GeophysicalUnion, Baltimore, MD, May 28-June 1, 1991.

MOORE, T.E. ES53Origins of Magnetospheric Plasma. Forpublication in Reviews of Geophysics,Washington, DC.

MOREL, D.E.STEFANESCU, D.M.DIAMOND, S.RUSSELL, K.C.

ES75

CURRERI, P.A.The Role of Gravity in MicrostructuralDevelopment in Particular Reinforced MetalMatrix Composites. For presentation at the23rd International SAMPE TechnicalConference, Kiamesha Lake, NY, October22-24,1991.

MORTON, C. ES75HOFMEISTER, W.H.BAYUZICK, R.J.ROBINSON, M.B.

Statistical Analysis of NucleationTemperatures From Two ContainerlessProcessing Methods. For presentation at theFourth International Symposium onExperimental Methods for MicrogravityMaterials Science, Research, San Diego,CA, March 1-5,1992.

MUSffiLAK, Z.E. ES52FONTENLA, J.M.MOORE, R.L.

Klein-Gordon Equation and Reflection ofAlfven Waves in Nonuniform Media. Forpublication in Physics of Fluids B,Woodbury, NY.

NEAL, V. ES63FISHMAN, G.KNIFFEN, D.

Gamma-Ray Observatory: The Next GreatObservatory in Space. For publication inMercury, San Francisco, CA.

NEIN, M.E. PS02DAVIS, B.

System Concepts for a Large UV/Optical/IRTelescope on the Moon. For presentation atthe Space Astronomical Telescopes andInstruments sponsored by SPIE, Orlando,FL, April 1-5,1991.

NEIN, M.E. PS02DAVIS, B.

A Large UV/Optical/IR Telescope on theMoon. For presentation at the 28th SpaceCongress, Cocoa Beach, FL, April 23-26,1991.

NERNEY, S. ES52SUESS, S.T.

Correction to "Flow Downstream of theHeliospheric Terminal Shock, 1: Irrotational

50

Page 56: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Flow." For publication in The Journal ofGeophysical Research, Washington, DC.

NERNEY, S. ES52SUESS, S.SCHMAHL, E.J.

Flow Downstream of the HeliosphericTerminal Shock: Magnetic Field Kinematics.For publication in Astronomy andAstrophysics, Meudon, France.

NETTLES, A.T. EH33LANCE, D.G.

A Study of the Damage ToleranceEnhancement of Carbon/Epoxy Laminated byUtilizing an Outer Lamina of Ultra HighMolecular Weight Polyethylene. Forpresentation at the 23rd InternationalSAMPE Technical Conference, LakeKiamesha, NY, October 22, 1991.

NETTLES, A.T. EH33HODGE, A.J.

Compression-After-Impact Testing of ThinComposite Materials. For presentation atthe 23rd International, SAMPE TechnicalConference, Lake Kiamesha, NY, October22-24,1991.

NETTLES, A.T. EH33LANCE, D.G.HODGE, A.J.

A Damage Tolerance Comparison of 7075 -T6 Aluminum Alloy and IM7/977-2Carbon/Epoxy. For presentation at the 36thInternational SAMPE Symposium, SanDiego, CA, April 15-18, 1991.

NOEVER, D.A. ES76Self-Collapse of Protein Crystals: ScalingRelations for Structural Fragility. Forpresentation at the Fourth InternationalConference on Crystallization of BiologicalMacromolecules, Freiburg, Germany, August18-23,1991.

NOEVER, D.A. ES76CRONISE, R.J.

Gravity Coarsening of Bubble Lattices. Forpresentation at the Fifth Annual MeetingAlabama Materials Research Conference,Birmingham, AL, September 25-26,1991.

NOEVER, D.A. ES76CRONISE, R.J., IV

Gravity Coarsening of Bubble Lattices. Forpresentation at the Gordon ResearchConference, Plymouth, NH, June 17-21,1991.

NOEVER, D.A. ES76Size Effects and Failure Model forMechanically Stressed Protein Crystals andAggregates. For presentation at the FourthInternational Conference on Crystallizationof Biological Macromolecules, Freiburg,Germany, August 18-23, 1991.

NOEVER, D.A. ES76Statistics of Contractive Cracking Patterns.For publication in Canadian Journal ofPhysics, Quebec, Canada.

NOEVER, D.A. ES76Fractal Dimension of BioconvectionPatterns. For publication in Journal of thePhysical Society of Japan, Tokyo, Japan.

NOEVER, D.A. ES76Rotating Bioconvection: A New Twist onLife. For publication in American Journal ofPhysics, Wooster, MA.

NOEVER, D.A. ES76Diffusive Slip and Surface TransportProperties. For publication in Journal ofColloid and Interfacial Science, New York,NY.

NOEVER, D.A. ES76Evolution of Bioconvective Patterns inVariable Gravity. For publication in ThePhysical Review A15, Ridge, NY.

NOEVER, D.A. ES76Aggregative Stability in Lecithin Liposomes:A Statistical Crystallographic Approach. Forpublication in Journal of Colloid andInterfacial Science, New York, NY.

NOEVER, D.A. ES76A 3/2 Power Law Spanning MultipleBioconvective Planforms. For publication inPhysical Review Letters, Ridge, NY.

51

Page 57: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

NOEVER, D.A. ES76Statistics of Pre-Mixed Flame Cells. Forpublication in The Physical Review A15,Ridge, NY.

NOEVER, D.A. ES76Statistics of Low-Density MicrocellularMaterials. For publication in Journal ofMaterials Science, New York, NY.

NOLL, K.S. ES63The Strange Gases of Jupiter and Saturn. Forpublication in The Planetary Report,Pasadena, CA.

NOLL, K.S. ES63Saturn's Great White Spots: CorrelationWith Heliocentric Distance. For publicationin Nature, Washington, DC.

NUNES, A.C., JR. EH42Modeling the VPPA Welding Process. Forpresentation at the Advanced AerospaceMaterials/Processes (Aeromat) Conferenceand Exposition, Long Beach, CA, May 20-24, 1991.

NURRE, G.S. ED12SHARKEY, J.P.WAITES, H.B.

Initial Performance Improvements Due toDesign Modifications for the Pointing ControlSystem on the HST. For presentation at the14th Annual AAS Guidance and ControlConference, Keystone, CO, February 2-6,1991.

NURRE, G.S. ED 12In-Flight Experience and Lessons Learnedon HST. For presentation at Dynamics andControl of Flexible Aerospace Structures:Modeling and Verification, InternationalFederation of Automatic Control, Huntsville,AL, April 2-4, 1991.

OBENHUBER, D.C. EH32SHAFFER, J.BRITTAIN, A.RODGERS, E.G. EH32

Closed Ecological Systems as Models forLong-Term Life Support Systems. Forpresentation at the Seventh Annual Ameri-can Society of Gravitational and Space Biol-ogy, Washington, DC, October 17-20,1991.

OLSEN, C.D. EO43ECHOLS, R.T.WOODS, W.K.ONKEN, J.F.

Orbiter Attitude Design for the Astro-1Spacelab Mission. For presentation at theAIAA Space Programs and TechnologiesConference, Huntsville, AL, March 24-27,1992.

OSHEROVICH, V.A. GSFCGARCIA, H.A. NOAAHAGYARD, M.J. ES52

Three-Component Electric Current Densityin a Unipolar Sunspot With Twisted Field.For presentation at the Meeting of theAmerican Astronomical Society/SolarPhysics Division, Huntsville, AL, April 9-12,1991.

OWENS, J.K. ES55TORR, M.R.

Emissions From the 4-5 eV 02 States in theTerrestrial Nightglow. For presentation atthe 1991 Spring Meeting of the AmericanGeophysical Union, Baltimore, MD, May 28-June 1,1991.

PAIK, HJ. ES01MORGAN, S.H.

Superconducting Gravity GradiometerMission. For publication in the Proceedingsof The First William Fairbanks Meeting onRelativistic Gravitational Experiments inSpace, University of Rome, Rome, Italy,September 10-14, 1990.

PALEY, M.S. ES74FRAZIER, D.O.ABELEDEYEM, H.McMANUS, S.P.ZUTAUT, S.E.

Synthesis, Vapor Growth, Polymerization,and Characterization of Thin Films of NovelDiacetylene Derivatives of Pyrrole. The Useof Computer Modeling to Predict Chemicaland Optical Properties of TheseDiacetylenes and Polydiacetylenes. Forpublication in Journal of the AmericanChemical Society, Austin, TX.

52

Page 58: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

PANG, Q.PANG, T.NUNES, A.C. EH42McCLURE, J.

Workpiece Cleaning During Variable PolarityPlasma Arc Welding of Aluminum. Forpublication in ASME Journal of Engineeringfor Industry, New York, NY.

PARNELL, T.A. ES62ASAKIMORI, K.DERRICKSON, J.H.FOUNTAIN, W.F.FUKI, M.et al.

SCIN/MAGIC: Spectra, Composition, andInteractions of Nuclei With a Balloon-BorneSuperconducting Magnet. For presentationat the 22nd International Cosmic Ray Con-ference, Dublin, Ireland, August 11-23, 1991.

PARNELL, T.A. ES62WATTS, J.W., JR.BENTON, E.V.DUDKIN, V.E.KOVALEV, E.E.BENTON, E.R.et al.

Cosmic Ray LET Spectra and Doses onBoard COSMOS-2044 Biosatellite. Forpublication in Nuclear Track and RadiationMeasurements, Pergamon Press, Oxford,England.

PARNELL, T.A. ES62Summary of Ionizing Radiation Analysis onthe Long Duration Exposure Facility. Forpresentation at the First LDEF PostRetrieval Symposium, Orlando, FL, June 2-8,1991.

PATEL, S. PP03Predicting the Cost of NASA SpacePrograms Using Historical Cost Trends. Forpresentation at the Society of WomenEngineers National Convention, San Diego,CA, June 25-29, 1991.

Electron Mobility in n-Type Hg!_xCdxTeand Hg t_xZnxTe Alloys. For publication inJournal of Applied Physics, New York, NY.

University of Iowa

Lockheed

Phillips

PATTERSON, J.D.ABDELHAKIEM, W.LEHOCZKY, S.L.

ES75

PERSOON, A.M.ANDERSON, R.R.PETERSON, W.K.. .COLLIN, H.L.ROBINSON, R.M.SINGER, H.J.KERNS, K.HARDY, D.A.DENIG, B.MAYNARD, N.C.WYGANT, R., JR. University of CaliforniaSLAVIN, J.A. GSFCPOLLOCK, C.J. ES53MOORE, T.E. ES53

Observations of a Quiet Magnetosphere andPolar Cap by CRRES, DE-1, and DMSP. Forpresentation at the 1991 Fall AGU Meeting,San Francisco, CA, December 9-13, 1991.

PETERS, P.N. ES63CRISTL, L.GREGORY, J.C.

Measurements of Erosion Characteristics forMetal and Polymer Surfaces Using Pro-filometry. For publication in Conference Pro-ceedings of the First LDEF Post RetrievalSymposium, Orlando, FL, June 1991.

PETERS, P.N. ES63GREGORY, J.C.

Pinhole Cameras: Multipurpose Sensors forAtomic Oxygen in Orbit; Application toAttitude Determination of the LDEF. Forpublication in Conference Proceedings of theFirst LDEF Post Retrieval Symposium,Orlando, FL, June 1991.

PETERS, P.N. ES63GREGORY, J.C.LIGIA, C.C.RAIKAR, G.

Effects on LDEF Exposed Copper Film andBulk. For publication in ConferenceProceedings of the First LDEF PostRetrieval Symposium, Orlando, FL, June1991.

53

Page 59: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

POLITES, M.E. ED10Reconstructing Tethered Satellite SkipropeMotion by Bandpass Filtering Magne-tometer Measurements. For publication inJournal of Spacecraft and Rockets,Washington, DC.

POLITES, M.E. ED12A New Scheme for Processing Star TrackerMeasurements in Spacecraft AttitudeDetermination Systems. For presentation atthe AIAA Guidance, Navigation, and ControlConference, New Orleans, LA, August 12-14,1991.

PORTER, J.G. ES52HOOVER, R.B.WALKER, A.B.C.

The Quiet Solar Network at 10 6 K. Forpresentation at the Gordon ResearchConference, Plymouth, NH, August 5-9,1991.

PORTER, J.G. ES52FONTENLA, J.M.MOORE, R.L.SIMNETT, G.M.

The X-Ray Counterparts of UV Microflares.For presentation at the AAS-Solar PhysicsDivision and MAX '91 Meeting, Huntsville,AL, April 9-12,1991.

PORTER, J.G. ES52FONTENLA, J.M.MOORE, R.L.SIMNETT, G.M.

Simultaneous UV and X-Ray Observationsof Solar Microflares. For presentation at the178th Meeting of the American AstronomicalSociety, Seattle, WA, May 26-30, 1991.

POULIN, E.HORAN, C. ED64

High Conductance Thermal Interface forSpace Applications. For presentation at the21st International Conference onEnvironmental Systems, San Francisco, CA,July 15-18,1991.

PREECE, R.D. ES62HARDING, A.K.

A Strong-Field Synchrotron Self-ComptonGamma-Ray Burst Emission Model. Forpresentation at the 22nd ICRC Dublin

Institute for Advanced Studies, Dublin,Ireland, August 12-23,1991.

PREECE, R.D. ES62HARDING, A.

Resonant Compton Cooling and AnnihilationLine Production in Gamma-Ray Bursts. Forpublication in The Astrophysical Journal,Tucson, AZ.

PRESTWICH, A.H. ES65WRIGHT, G.S.JOSEPH, R.D.

Variability of Near Infrared Emission Linesin NGC 4151—Implications for Nuclear StarFormation in Seyfert, Galaxies. Forpublication in The Astrophysical Journal,Chicago, IL.

PUSEY, M.L. ES76Continuing Adventures With LysozymeCrystal Growth. For presentation at theFourth International Conference on Crystal-lization of Biological Macromolecules,Freiburg, Germany, August 18-23, 1991.

PUSEY, M.L. ES76CACIOPPO, E.

The Effects of Acid Treatment and CalciumIons on the Solubility of Concanavalin A. Forpublication in the Conference Proceedings ofthe Fourth International Symposium on theCrystallization of Biological Macromolecules,Freiburg, Germany, August 18-23, 1991.

PUSEY, M.L. ES76Effects of Convection on Protein CrystalGrowth. For presentation at the PittsburghDiffraction Conference, Huntsville, AL,October 31-November 2,1990.

RAMACHANDRAN, N. ES42DOWNEY, J.P.

Three Dimensional Numerical Investigationof Gravitational and Solutal Effects in aCylindrical Cell. For presentation at theAIAA 26th Thermophysics Conference,Honolulu, ffl, June 24-26,1991.

RAMSEY, B.D.AUSTIN, R.A.BOWER, C.R.DJJETZ, K.L.FULTON, A.

ES65

54

Page 60: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

JOY, M.K.WEISSKOPF, M.C.

The MSFC Fluorescence-Gated ImagingProportional Counter. For presentation atSPIE's 1991 International Symposium, SanDiego, CA, July 21-26,1991.

REASONER, D.L. ES53The Chemical Release Mission of CRRES.For publication in Journal of Spacecraft andRockets, Washington, DC.

REASONER, D.L. ES53The First CRRES Chemical ReleaseCampaigns—Kwajalein, South Pacific, andHigh-Altitude Magnetosphere. Forpresentation at the 1991 Spring MeetingAmerican Geophysical Union, Baltimore,MD, May 28-June 1,1991.

RICHARDS, D.R. SverdrupCHARKLWICK, D.M. EP62

Investigation of Ice Formation in the SpaceShuttle Main Engine (SSME) 0209 MainInjector Coolant Cavity. For presentation atthe 27th Joint Propulsion Conference,Sacramento, CA, June 24-27, 1991.

ROBERTSON, F.R. ES42Consistency Between SSM/I-DerivedGlobal Moisture Analyses and Estimates ofLarge-Scale Vertical Motion. Forpresentation at the Sixth Conference onSatellite Meteorology and Oceanography,Atlanta, GA, January 5-10, 1992.

ROBERTSON, F.R. ES42CHRISTY, J.R.

Structure, Propagation, and Growth Rates ofTransient Anomalies in the TroposphericTemperature Field as Depicted by MSU2.For presentation at the Sixth Conference onSatellite Meteorology and Oceanography,Atlanta, GA, January 5-10, 1992.

ROBERTSON, F.R. ES42Low Frequency Variability in SSM/IMoisture Retrievals. For presentation at theNinth Conference on Numerical Weather

. Prediction, Denver, CO, October 14-18,1991.

ROBINSON, M.B.HOFMEISTER, W.H.

ES75

BAYUZICK, R.J.RATNZ, T.J.

Measurement of the Solidification Velocity inan Undercooled Free Falling Droplet. Forpresentation at the Fourth InternationalSymposium on Experimental Methods forMicrogravity Materials Science Research,San Diego, CA, March 1-5, 1992.

ROBSON, R.R. ES53WILLIAMSON, W.S.OLSEN, R.C.MOORE, T.E.

Plasma Contractor for the ISTP/POLARSpacecraft. For presentation at the 22ndInternational Electric Propulsion Conference,Centre Congressi, Viareggio, Italy, October14-17, 1991.

RODGERS, E.B. EH32OBENHUBER, D.C.

Closed Ecological Systems as Models forSpace Station. For presentation at TABES,Huntsville, AL, May 15, 1991.

RODGERS, E.B. EH32Ecology of Microorganisms in a ClosedSystem. For presentation at the Fifth AnnualSkin in Space Seminar, Huntsville, AL,October 17, 1991.

RODGERS, E.B. EH32Microbial Contamination of theEnvironmental Control and Life SupportSystem Water Recovery Test for SpaceStation. For presentation at the InternationalConference on Environmental Systems, SanFrancisco, CA, July 15-18, 1991.

RODGERS, E.B. EH32Microbial Contamination in NASA-Environmental Control and Life SupportSystem Water Recovery Test for SpaceStation Freedom. For presentation at theAmerican Society for Microbiology, Dallas,TX,May 12-16,1991.

RODGERS, E.B. EH32Microbial Starvation Survival of NineBacterial Cultures for Over 1 Year inDistilled Deionized Water. For presentationat the American Society of Microbiology,Dallas, TX, May 12-16, 1991.

55

Page 61: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

RODGERS, E.B. EH32Bioburden Control for Space StationFreedom's Ultrapure Water System. Forpresentation at the International Conferenceon Environmental Systems, San Francisco,CA, July 15-18, 1991.

RODRIGUEZ, P. ED52Optimum Design of a Linearly TaperedLaminated Orthotropic Cantilever Beam. Forpresentation at OPTI '91, Boston, MA, June25-27,1991.

ROMAN, M. ED62RODGERS, E.WILSON, M.E. BoeingOBENHUBER, D.HUFF, T.TERRELL, D.GAUTHIER, J.J.

Microbial Contamination in NASA ECLSSWater Recovery System Test. Forpresentation at the American Society ofMicrobiology 91st Annual Meeting, Dallas,TX, May 5-9,1991.

RONAN, R. ES52WEST, E.A.HAGYARD, M.J.BALASUBRAMANIAM, K.S.et al.

A Comparison of Vector MagnetogramsFrom the Marshall Space Flight Center andMees Solar Observatory. For publication inSolar Physics, The Netherlands.

ROSNER, R. ES52AN, C.-H.MUSJELAK, Z.E.MOORE, R.L.SUESS, S.T.

Magnetic Confinement, Alfven WaveReflection, and the Origins of X-Ray andMass Loss "Dividing Lines" for Late-TypeGiants and Supergiants. For publication inThe Astrophysical Journal Letters, Chicago,n.

ROTHERMEL, J.JONES, W.SRIVASTAVA, V.JARZEMBSKI, M.HAMPTON, D.

ES43

Remote Tropospheric Backscatter Measure-ments at 9.1 and 10.6 Micrometers WithAirborne Focused Doppler Lidars. Forpresentation at the Coherent Laser RadarTopical Meeting, Snowmass, CO, July 8-12,1991.

RUSSELL, C. EH42POORMAN, R.JONES, C.S.NUNES, A.HOFFMAN, D.

Considerations of Metal Joining Processesfor Space Fabrication, Construction, andRepair. For presentation at the 23rdInternational SAMPE Technical Conference,Kiamesha Lake, New York, October 22-24,1991.

RUSSELL, S.S. EH13Technical Material on Impacts of CompositeMaterials Which Were Acquired FromApplicants University Research, NDE ofImpact Damage to Fibrous Composites. Forpresentation at the NondestructiveEvaluation for Aerospace Requirements,Huntsville, AL, June 4-6, 1991.

SAFIE, P.M. CT13FOX, E.P.

A Probabilistic Design Approach for LaunchSystems. For presentation at the 27thAIAA/SAE/ASME Joint PropulsionConference, Sacramento, CA, June 24-27,1991.

SAKURAI, H. ES65RAMSEY, B.D.

Dependence of Energy Resolution on AnodeDiameter in Xenon Proportional Counters.For publication in Nuclear Instruments andMethods in Physics, The Netherlands.

SAKURAI, H. ES65RAMSEY, B.D.

The Energy Resolution of a High-PressureXenon-Filled Proportional Counter. Forpresentation at the 1991 IEEE NuclearScience Symposium, Santa Fe, NM,November 5-8,1991.

SAKURAI, H.RAMSEY, B.D.WEISSKOPF, M.C.

ES65

56

Page 62: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

High Pressure Xenon Proportional Counterup to 10 atm. For publication in NuclearInstruments and Methods in PhysicsResearch, The Netherlands.

SAKURAI, H. ES65RAMSEY, B.D.

Characteristics of a High Pressure GasProportional Counter Filled with Xenon. Forpresentation at SPIE's 1991 InternationalSymposium on Optical Applied Science andEngineering, San Diego, CA, July 21-26,1991.

SCHARFEN, G.R. ES44GOODMAN, S.J.

Global Nighttime Lightning Detection FromDMSP Imagery. For presentation atIUGG/IAMAP Symposium, Vienna, Austria,August 11-24, 1991.

SCHMIEDER, B. ES52FONTENLA, J.TANDBERG-HANSSEN, E.

A Microflare-Related Activation of aFilament Observed in Hot and C IV Lines.For publication in Astronomy andAstrophysics, The Netherlands.

SCHUTZENHOFER, L.A. ED32McCONNAUGHEY, P.K.McCONNAUGHEY, H.V.WANG, T.S.

Management of a CFD Organization inSupport of Space Hardware Development.For presentation at the AIAA 22nd FluidDynamics, Plasma Dynamics, and LasersConference, Honolulu, HI, June 24-26,1991.

SHEPHERD, C.C. CQ24Marshall Space Flight Center Standard forElectrostatic Discharge (BSD) Control forPropellant and Explosive Devices. Forpresentation at the JANNAF PropulsionSystems Hazards Subcommittee Meeting,Albuquerque, NM, March 18-22, 1991.

SIBJLLE, L. ES76PUSEY, M.L.

Investigation Into the Early Stages ofLysozyme Nucleation. For publication inProceedings of Fourth International Confer-ence on Crystallization Growth of BiologicalMacromolecules, Freiburg, Germany.

SIMS, P.A. EP62ZEE, R.

Stress State in Turbopump Bearing Inducedby Shrink Fitting. For presentation at theAIAA/SAE/ASME Joint PropulsionConference, Sacramento, CA, June 24-27,1991.

SMITH, D. EL56PEARSON, S.

A Systems Engineering Approach toElectromagnetic Compatibility (EMC)Analysis for the Space Station FreedomProgram. For presentation at theElectromagnetic Compatibility Expo,Orlando, FL, June 25-27,1991.

SNODDY, W.C. PA01Geostationary Earth Observatories—KeyElements to Mission to Planet Earth. Forpresentation at the International Pacific Airand Space Technology (IPAQ Conference,Gifu, Japan, October 6-11,1991.

SNYDER.R.S. ES71PUSEY, M.CARTER, D.etal.

Protein Crystal Growth in Microgravity. Forpresentation at the IKI/AIAA MicrogravityScience Symposium, Moscow, Russia, May13-17, 1991.

SNYDER, R.S. ES75TAYLOR, W.WJLLENBERG, H.J.

Space Station Freedom Capabilities forUsers. For publication in Space TechnologyInternational, London, England, January1992.

SNYDER, R.S. ES71RHODES, P.H.

Electrophoresis Experiments in Micro-gravity. For presentation at the IKI/AIAAMicrogravity Science Symposium, Moscow,Russia, May 13-17, 1991.

SNYDER, R.S. ES76FURHMANN, K.WALTER, H.U.

Protein Crystallization Facilities forMicrogravity Experiments. For publication in

57

Page 63: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Journal of Crystal Growth, Amsterdam, TheNetherlands.

SPENCER, R.W. ES43CHRISTY, J.R.

A Physical Interpretation of BrightnessTemperatures Observed by the MicrowaveSounding Units Based on Raobs. Forpresentation at the Fifth Conference onClimate Variations, Denver, CO, October13-18,1991.

SPENCER, R.W. ES43CHRISTY, J.R.

Precision and Radiosonde Validation ofSatellite Gridpoint Temperature Anomalies,Part II: A Tropospheric Retrieval and TrendsDuring 1979-90. For publication in Journal ofClimate, Boston, MA, April 1991.

SPENCER, R.W. ES43CHRISTY, J.R.

Precision and Radiosonde Validation ofSatellite Gridpoint Temperature Anomalies,Part I: MSU Channel 2. For publication inJournal of Climate, Boston, MA, April 1991.

SPRINGER, J. ES74SILBERMAN, E.KROES, R.REISS, D.

Mapping Crystal Defects With a DigitalScanning Ultramicroscope. For presentationat SPIE's 36th Annual InternationalSymposium, San Diego, CA, July 21-26,1991.

STORY, G. SverdrupWILLIAMS, W. ED62

Space Station Freedom Water RecoveryTest Data Base. For presentation at theSAE ICES Convention, San Francisco, CA,July 15, 1991.

SU, C-H. ES75LEHOCZKY, S.L.SZOFRAN, F.R.GILLIES, D.G.PERRY, G.L.E.

Directional Solidification and Casting ofHgCdTe in a Transverse Magnetic Field. Forpresentation at the ECCG-3 Third EuropeanConference on Crystal Growth, Budapest,Hungary, May 5-11, 1991.

SUESS, S.T. ES52NERNEY, S.

The Magnetic Field in the Heliosheath. Forpresentation at Solar Wind Seven, Goslar,Germany, September 16-20, 1991.

SUESS, S.T. ES52MHD Flows in the Heliosphere. Forpublication in Reports on Astronomy(International Astronomical Union), TheNetherlands.

SUESS, S.T. ES52Dynamics of the Outer Heliosphere andTemporal Variations in the TerminationShock. For presentation at the 1991 FallMeeting of the American Geophysical Union,San Francisco, CA, December 9-13, 1991.

SUESS, S.T. ES52Shape of and Plasma Flow Patterns Aroundthe Heliopause. For presentation at theEuropean Geophysical Society 16th GeneralAssembly, Wiesbaden, Germany, April 22,1991.

SUITS, M.W. EH13Air Coupled Ultrasonic Inspection of LargeSolid Rocket Motors. For presentation at theNondestructive Evaluation for AerospaceRequirements, Huntsville, AL, June 4-6,1991.

SULLIVAN, K.W. EE74SCHRAMM, F. PF24

An Evaluation of the Total QualityManagement Implementation Strategy forASRM at NASA/MSFC. For presentation atthe University of Tennessee Space InstituteMasters Degree Thesis, Tullahoma, TN,March 1991.

SULYMA, P.R.REARDON, J.E.EVERSON, J.SMITH, S.D.

ED33RemtechRemtech

SECAASRM Radiation and Flowfield Status. Forpresentation at the JANNAF PlumeTechnology Conference, Redstone Arsenal,AL, May 14-16, 1991.

SUSKO, M. ES44Chemical Analysis Reveals the DifferenceBetween Natural and Manmade Space

58

Page 64: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Debris. For publication in GeophysicalResearch Letters, Washington, DC.

SUSKO, M. ES44Turbulence Indicators for Space ShuttleLaunches. For presentation at the AIAA30th Aerospace Sciences Meeting andExhibit, Reno, NV, January 6-9, 1992.

TAKAHASHI, Y. ES62GREGORY, J.C.HAYASHI, T.CHRISTL, M.J.DERRICKSON, J.H.FOUNTAIN, W.F.PARNELL, T.A.etal.

A Study of Isospin Clustering andIntermittency Fluctuations in Heavy IonReactions From CERN EMU05. Forpresentation at the 22nd InternationalCosmic Ray Conference, Dublin, Ireland,August 11-23, 1991.

TANDBERG-HANSSEN, E. ES01FONTENLA, J.M.

X. Prominences. For presentation at the 21stIAU General Assembly, Buenos Aires,Argentina, July 23-August 1, 1991.

TAYLOR, W. ES71SNYDER, R.WILLENBERG, H.

Space Station Freedom Capabilities forUsers. For presentation at the 42ndCongress of the International AstronauticalFederation, Montreal, Canada, October 5-11, 1991.

TELESCO, C.M. ES63KNACKE, R.F.

Detection of Silicates in the p Pictoris Disk.For publication in Astrophysical JournalLetters, Cambridge, MA.

THOMAS, F. ED52Slip Joint Invention. For publication inDesign News Excellence in DesignCompetition, Chicago, IL, February 24-27,1992.

Mechanical Joint Development Testing forIn-Space Assembly and Construction. Forpresentation at the AIAA Space Programsand Technologies, Huntsville, AL, March 24-27,1992.

THRASHER, D. BoeingDAVISON, G.TUCKER, M. PS04

Space Station Evolution Logistics. Forpresentation at the Society of Allied WeightEngineers, Guntersville, AL, October 6,1990.

THREET, G.E., JR. PD24PANNELL, W.P.

ET Derived Core Stage. For presentation atthe 28th Space Congress, Cocoa Beach, FL,April 23-26, 1990.

TINKER, M.L. ED22CLAYTON, J.P. Remtec

Characterization and Modeling of AdvancedCeramic Fabric for Space Applications. Forpresentation at the AIAA 32nd StructuresStructural Dynamics and Materials Con-ference, Baltimore, MD, April 8-10, 1991.

TORR, M.R. ES51TORR, D.G.SPANN, J.OWENS, J.SAVAGE, L.FELLOWS, C.etal.

Optical Observations of a Lithium ReleaseFrom the CRRES Spacecraft. Forpresentation at the Spring 1991 Meeting ofthe American Geophysical Union, Baltimore,MD, May 28-30, 1991.

TORR.M. ES51TORR, D.G.ZUKIC, M.SPANN, J.

An Ultraviolet Imager for the InternationalSolar-Terrestrial Physics Mission. Forpublication in Reviews of ScientificInstruments, Woodbury, NY.

THOMAS, P.P.FINCKENOR, J.L.

ED52TORR, M.TORR, D.G.RICHARDS, P.O.

ES51

59

Page 65: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

The N2+ First Negative System in theDayglow From Spacelab 1. For publication inJournal of Geophysical Research,Washington, DC.

TORRES, M.R. EH42McCLURE, J.C.NUNES, A.C.GUREVITICH, A.C.

Gas Contamination Effects in VariablePolarity Plasma Arc Welding. For publicationin Welding Journal, Miami, FL.

TRAWEEK, M.S. ED62Space Station Water Recovery Design andTest. For publication in Processing in SpaceWaste Management and Research, MoffettField, CA.

TRAWEEK, M.S. ED62BAGDIGIAN, R.M.GRIFFITH, G. Sverdrup

Phase III Integrated Water RecoveryTesting at MSFC: Partially Closed LoopResults and Lessons Learned. Forpresentation at the 21st IntersocietyConference on Environmental Systems, SanFrancisco, CA, July 15-18, 1991.

TUCKER, D.S. EH34Long-Life Prediction of Glass in Space. Forpublication in SAMPE Local ChapterProceedings, Huntsville, AL, March 22,1991.

TUCKER, D.S. EH34ETHRIDGE, E.G.CURRERI, P.A.

Production of Continuous Glass Fiber UsingLunar Simulant. For presentation at the 23rdAnnual SAMPE Technical Conference, LakeKiamesha, NY, October 22-24, 1991.

UPADHYAY, T.N. EL58COTTERILL, S.DEATON, A.W. EL58

Autonomous Reconfigurable GPS/INSNavigation and Pointing System forRendezvous and Docking. For presentationat the Automated Rendezvous and CaptureReview, Williamsburg, VA, November 19-21, 1991.

UPADHYAY, T. MCCICOTTERILL, S. MCCIDEATON, A.W. EL58

Autonomous GPS/INS NavigationExperiment for Space Transfer Vehicle(STV). For presentation at the First ESAInternational Conference on SpacecraftGuidance, Navigation, and Control Systems,Noordwijk, The Netherlands, June 4-7, 1991.

UPADHYAY, T. MCCIRHODEHAMEL, H. MCCIDEATON, A.W. EL58

Navigation With Lunar-Based GPSPseudolites. For presentation at the 1stESA International Conference on SpacecraftGuidance, Navigation, and Control Systems,Noordwijk, The Netherlands, June 4-7, 1991.

UTREJA, L. ED12CHRISTIAN, P.M.BUKLEY, A.

Multibody Modeling Verification and Control.For presentation at the AAS/AIAA SpaceFlight Mechanics Meeting, ColoradoSprings, CO, February 24-26, 1991.

VAUGHAN, O.K. ES43Photograph and Caption. For publication inAMS Journal, September 9, 1991, CoverPhotograph, Boston, MA.

VAUGHN, J.A. EH12CARRUTH, M.R., JR.

Current Flow in a Plasma Caused byDielectric Breakdown. For presentation atthe Space Operations, Applications, andResearch Symposium 1991, Houston, TX,July 9-11,1991.

VENKATESWARLU, P. ES74HE, K.BRYANT, W.HYDE, H.PENN, B.FRAZIER, D.

New Organic Materials for Nonlinear Optics:Study of High Efficient Second HarmonicGeneration From N-Alkyl and N,N-DialkylDerivatives of 4-Methyl-6-Mitro-2-Quinolinamines. For presentation at CLEO91, Baltimore, MD, May 12-17, 1991.

60

Page 66: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

VERDERAIME, V. ED01Aerostructural Safety Factor SelectionCriterion. For presentation at the AIAASpace Programs and TechnologiesConference, Huntsville, AL, March 24-27,1992.

VIKRAM, C.S. ES74WITHEROW, W.K.TROLINGER, J.D.

Refractive Properties of TGS AqueousSolution for Two-Color Interferometry. Forpresentation at SPIE's InternationalSymposium, San Diego, CA, July 21-26,1991.

VIKRAM, C.S. UAHWITHEROW, W.K. ES74TROLINGER, J.D.

Determination of Refractive Properties ofFluids for Dual Wavelength Interferometry.For publication in Applied Optics, NewtonHighlands, MA.

VOLZ, M.P. ES75SU, C.-H.LEHOCZKY, S.L.SZOFRAN, F.R.

Vibronic Spectra of Cu2+ In ZnTe. Forpublication in Physical Review B, New York,NY.

VON PRAGENAU, G.L. ED14Damping Bearings for Cryogenic Turbo-pumps. For presentation at the 1990JANNAF Propulsion Meeting, Anaheim, CA,October 3-5, 1990.

WATTES, H.B. ED12Challenges to Performance. For presentationat Dynamics and Control of FlexibleAerospace Structures: Modeling andVerification, International Federation ofAutomatic Control, Huntsville, AL, April 2-4,1991.

WALKER, A.B.C., JR. ES52HOOVER, R.B.etal.

High Resolution Imaging With MultilayerSoft X-Ray, EUV, and FUV Telescopes ofModest Aperture and Cost. For publicationin Optical Engineering, Bellingham, WA.

WALKER, A.B.C., JR. ES52LINDBLOM, J.L.TIMOTHY, J.G.HOOVER, R.B.

The Ultra High Resolution XUV TelescopeIII: A Modified Configuration for a FreeFlying Platform. For presentation at SPIE'sMultilayer and Grazing Incidence X-RayEUV Optics, San Dieco, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52KANKELBORG, C.HOOVER, R.B.etal.

Narrow Band Solar Images in the Soft X-Ray (-5-50A) Regime With MultilayerOptics. For presentation at SPIE'sMultilayer and Grazing Incidence X-RayEUV Optics, San Diego, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52MOORE, R.ROBERTS, W.HOOVER, R.B.etal.

The High Resolution Telescope Cluster. Forpresentation at SPIE's Multilayer andGrazing Incidence X-Ray EUV Optics, SanDiego, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52MARTINEZ, D.S.HOOVER, R.B.

Cosmic X-Ray Spectroscopy WithMultilayer Optics. For presentation atSPIE's Multilayer and Grazing Incidence X-Ray EUV Optics, San Diego, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52WILLIS, T.D.HOOVER, R.B.

The Objective Double Crystal Spectrometer.For presentation at SPIE's Multilayer andGrazing Incidence X-Ray EUV Optics, SanDiego, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52ALLEN, M.J.HOOVER, R.B.

Performance of Reflective Multilayer CoatedCoronagraphs. For presentation at SPIE's

61

Page 67: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

Multilayer and Grazing Incidence X-RayEUV Optics, San Diego, CA, July 21-26,1991.

WALKER, A.B.C., JR. ES52DeFOREST, C.E.BARBEE, T.W.HOOVER, R.B.

Design of a Normal Incidence XUV GratingSpectrograph Using Multilayer Techniques.For presentation at SPIE's Multilayer andGrazing Incidence X-Ray EUV Optics, SanDiego, CA, July 21-26, 1991.

WALKER, A.B.C., JR. ES52LINDBLOM, J.F.TIMOTHY, J.G.HOOVER, R.B.TANDBERG-HANSSEN, E.BARBEE, T.W., JR.

The Ultra High Resolution XUVSpectroheliograph. For presentation at theAAS-Solar Physics Division and MAX '91Meeting, Huntsville, AL, April 9-12, 1991.

WANG, M. EH13WORKMAN, G.L.BRYSON, C.

Eddy Current Analysis of Graphite FiberMaterials. For presentation at the AlabamaMaterials Research Conference, Tuscaloosa,AL, October 2-3, 1990.

WANG, T.-S. ED32SCHUTZENHOFER, L.

Numerical Analysis of a Nuclear ElementTester for Thermal Nuclear Propulsion. Forpresentation at AIAA/NASA/OAI Confer-ence on Advanced SEI Technologies,Cleveland, OH, September 4-6, 1991.

WANG, T.-S. ED32Numerical Study of the Transient NozzleFlow Separation of Liquid Rocket Engines.For presentation at the Fourth InternationalSymposium on CFD, Davis, CA, September9-12, 1991.

WANG, T.-S. ED32Computational Analysis of the Three-Dimensional Steady and Transient SSMEFuel Preburner Combustor. For presentationat the International Union of Theoretical andApplied Mechanics (IUTAM) Symposium on

Aerothermodynamics in Combustors, Taipei,Taiwan, R.O.C., June 3-5,1991.

WATTS, J. ES62LDEF Radiation Environment. Forpresentation to the NATO Advanced StudyInstitute, Algarve, Portugal, October 12,1991.

WATTS, J.W., JR. ES62DERRICKSON, J.H.PARNELL, T.A.FISHMAN, G.J.HARMON, A.BENTON, E.V.etal.

The Ionizing Radiation Environment ofLDEF Prerecovery Predictions. Forpresentation at the First LDEF Post-Retrieval Symposium, Orlando, FL, June 2-8,1991.

WEDDENDORF, B. ED52Portable Powered Seat Lift Design. Forpublication in Design News Magazine,Newton, MA, and Institute for TechnologyDevelopment, Oxford, MS.

WEISSKOPF, M.C. ES65The Advanced X-Ray Astrophysics Facility.For presentation at the Colloquium onAXAF, Toledo, OH, June 5-7, 1991.

WEISSKOPF, M.C. ES65ELSNER, R.F.

Off-Axis Effects in Focal Plane Stellar X-Ray Polarimeters. For presentation atSPIE's 1991 International Symposium, SanDiego, CA, July 21-26,1991.

WEST, E.A. ES52Problems Associated With Aligning MSFCTransverse Azimuth Maps and H-AlphaImages. For presentation at the AAS-SolarPhysics Division and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

WHTTAKER,A. EH11Preliminary Assessment of LEO SurfaceEffects on LDEF A0171 CompositeMaterials. For publication in AdvancedMaterials and Processing, April 1991.

62

Page 68: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

WHITAKER, A.F. EH 11YOUNG, L.E.

An Overview of First Results on Solar ArrayPassive Experiment (SAMPE) No. A0171.For presentation at the LDEF InvestigatorsWorking Group Meeting, Orlando, FL, June2-8,1991.

WHORTON, M.S. ED12Simulation of the IPS for the Astro-1Mission. For presentation at the AIAA 29thAerospace Sciences Meeting and Exhibit,Reno, NV, January 7-10, 1991.

WILFONG, T.L. ES44Improving the Velocity Estimates From theNASA 50 MHz Wind Profiler. Forpresentation at the Second Symposium onTropospheric Profiling, Boulder, CO,September 9-13, 1991.

WILFONG, T.L. ES44SMITH, S.A.

High Temporal Resolution VelocityEstimates From the NASA 50 MHz WindProfiler. For presentation at the AIAA 30thAerospace Sciences Meeting, Reno, NV,January 6-9, 1992.

WILKINSON, L.K. ES52The Distribution of Longitudinal Currents inSunspots. For presentation at the AAS-Solar Physics Division and MAX '91Meeting, Huntsville, AL, April 9-12, 1991.

WILLIAMS, R.W. ED32Computational Study of Duct and Pipe FlowsUsing the Method of Pseudocompressibility.For presentation at the AIAA 21st FluidDynamics, Plasma Dynamics, and LasersConference, Honolulu, HI, June 24-26,1991.

WILLIAMS, W. ED62STORY, G. SverdrupCHIU, C. ION

Space Station Freedom ECLSS Data BaseSystem (FEDS) for MSFC Testing. Forpresentation at the 21st IntersocietyConference on Environmental Systems, SanFrancisco, CA, July 15-18,1991.

Determination of Monomer Concentrations inCrystallizing Lysozyme Solutions. Forpublication in the Proceedings of the FourthInternational Conference on Crystallizationof Biological Macromolecules, Freiburg,Germany.

WILSON, R.B. ES62HARMON, B.A.FINGER, M.H.MEEGAN, C.A.FISHMAN, G.J.PACIESAS, W.S.

Long-Term Source Monitoring Capabilitiesof BATSE. For presentation at the Gamma-Ray Observatory Science Workshop,Annapolis, MD, September 23-25, 1991.

WILSON, R.M. ES52Using the "Even-Odd" Sunspot CycleVariation to Predict Maximum Amplitude forCycle 23. For presentation at the AAS-SolarPhysics Division and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

WINGARD, C.D. EH33PATTERSON, W.J.

The Use of Photoelectron Emission toDetermine the Effects of Contamination onBond Strength and Integrity ofMetal/Polymer Composite Specimens. Forpresentation at the American ChemicalSociety (National Meeting), Atlanta, GA,April 14-19,1991.

WINKLER, C.DAILEY, C.CUMINGS, N.

Advanced(AXAF)

TA71

WILSON, L.J.PUSEY, M.L.

ES76

X-Ray Astrophysics FacilityScience Instruments. For

presentation at SPIE's InternationalSymposium on Optical Engineering andPhotonics in Aerospace Sensing, Orlando,FL, April 1-5, 1991.

WINTER, C.A. ES42JONES, J.

A Data Base Describing Low Gravity Fluidsand Materials Processing Experiments. Forpresentation at the AIAA 30th AerospaceSciences Meeting, Reno, NV, January 6-9,1992.

63

Page 69: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

MSFC PAPERS CLEARED FOR PRESENTATION(Available only from authors. Dates are presentation dates.)

WITHEROW, W.K. ES74Visualizing Convection During CrystalGrowth. For presentation at the PittsburghDiffraction Conference, Huntsville, AL,October 31-November 2, 1990.

WITHEROW, W.K. ES74Measuring Residual Accelerations in theSpacelab Environment. For presentation atSPIE's 36th Annual InternationalSymposium, San Diego, CA, July 21-26,1991.

WOODIS, K. EH 13Overview of NDE Programs at MarshallSpace Flight Center. For presentation at theNondestructive Evaluation of AerospaceRequirements, Huntsville, AL, June 4-6,1991.

WORKMAN, G. EB24HINMAN, E.

Physical and Digital Simulations of Robotsfor Space. For presentation at SimTec 1991,Orlando, FL, October 21-23, 1991.

WORKMAN, G.L. EH13WANG, M.ADAMS, B.

Robotic Eddy Current Inspection for GraphiteFiber Components. For presentation at theThird Conference on NDE for AerospaceRequirements, Huntsville, AL, June 6, 1991.

WU, S.T. ES01SONG, M.T.TANDBERG-HANSSEN, E.

A Numerical Simulation of AtmosphericResponses Due to Emerging Flux FromSubphotospheric Layers. For presentation atthe 21st SPD Meeting of the AmericanAstronomical Society and MAX '91 Meeting,Huntsville, AL, April 9-12, 1991.

YOUNG, A.C. PD32EMRICH, W.J.MULQUEEN, J.A.

Nuclear Stage Configuration Studies forMars Missions. For presentation at the 28thSpace Congress, Cocoa Beach, FL, April 23-26,1991.

ZUKIC.M. ES51TORR, D.TORR, M.

High Throughput Narrowband 83.4 nm Self-Filtering Camera. For publication in OpticalEngineering, Bellingham, WA.

ZWIENER, J.M. EH15Unusual Materials Effects Observed on theThermal Control Surfaces Experiment No.S0069. For presentation at the LDEFInvestigators Working Group, Orlando, FL,June 2-8,1991.

64

Page 70: SAbeing evaluated using eddy current inspection techniques. The unique capabilities of E-probes and horseshoe probes for inspecting probes for inspecting graphite fiber materials have

APPROVAL

FY 1991 SCIENTIFIC AND TECHNICAL REPORTS,ARTICLES, PAPERS, AND PRESENTATIONS

Compiled by Joyce E. Turner

The information in this report has been reviewed for technical content. Review of anyinformation concerning Department of Defense or nuclear energy activities or programs hasbeen made by the MSFC Security Classification Officer. This report, in its entirety, has beendetermined to be unclassified.

C.D. BEANDirectorAdministrative Operations Office

U.S. GOVERNMENT PRINTING OFFICE 1992-631-060/60040

65