n94-28136 - nasa...systems, inc. ofi vibration the order of testing shall be z axis, then y axis,...

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J.. N94- 28136 _z =i 1.1.1 o3 1993 NASA Aerospace Battery Workshop -775- Advanced Technologies Session https://ntrs.nasa.gov/search.jsp?R=19940023633 2020-05-27T21:34:42+00:00Z

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Page 1: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

J.. •

N94- 28136

_z

=i1.1.1

o3

• • • •

1993 NASA Aerospace Battery Workshop -775- Advanced Technologies Session

https://ntrs.nasa.gov/search.jsp?R=19940023633 2020-05-27T21:34:42+00:00Z

Page 2: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

rd3

f_t',4

+'6r_

0

1993 NASA Aerospace Battery Workshop -776- Advanced Technologies Session

Page 3: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1993 NASA Aerospace Battery Workshop -777- Advanced Technologies Session

Page 4: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

ID

1993 NASA Aerospace Battery Workshop -778- Advanced Technologies Session

Page 5: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

¢-0

mm

0imm

Q.

_0_._,

IE0

O_

dz_o_

LU

>.U)

1993 NASA Aerospace Battery Workshop -779- Advanced Technologies Session

Page 6: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1993NASAAerospaceBatteryWorkshop -780- Advanced Technologies Session

Page 7: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

_.. 01 01 °i:::: r "T""_-. .:.- £:

"0--,

Qm _ _r->_o > >o

1993 NA Aerospace Battery Workshop -781- Advanced Technologies Session

Page 8: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

.C.

m

2

1993 NASA Aerospace Battery Workshop -782- Advanced Technologies Session

Page 9: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0• m g:

0

x-- Cx_

CD ="0 ,.,

CD

C

e_x...

G)4=

O

._._'-_

g ,___ _ "i

"_E.=_

1993 NASA Aerospace Battery Workshop -783- Advanced Technologies Session

Page 10: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0

0

i

0

0,1=

"00N

im

E|m

O.0

C|m

m000s_

13.

1993 NASA Aerospace Battery Workshop -784- Advanced Technologies Session

Page 11: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

m

e-

OW

" o.2 ._ o

. _m _E"_o E__o

o_ _ o_0 0 0 "_

1993 NASA Aerospace Battery Workshop -785- Advanced Technologies Session

Page 12: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

x_

c_z

1993 NASA Aerospace Battery Workshop -786- Advanced Technologies Session

Page 13: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

t,'s

1993 NASA Aerospace Battery Workshop -787- Advanced Technologies Session

Page 14: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

"3

Q

1993 NASA. Aerospace Battery Workshop -788- Advanced Technologies Session

Page 15: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

m

////////

--/

//

2_ °

1993 NASA Aerospace Battery Workshop -789, Advanced Technologies Session

Page 16: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

+

'i

÷

+ I

÷

1

, II t

I

I I

?

1993 NASA Aerospace Battery Workshop -790- Advanced Technologies Session

Page 17: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

!

1993 NASA Aerospace Battery Workshop -791- Advanced Technologies Session

Page 18: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0 "...,..

.-_/.i _/

/;

//

I

k/%

1993 NASA Aerospace Battery Workshop -792- Advanced Technologies Session

Page 19: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I

I

I

I I I

I

I

t

I

+

0

I

q

?..°

V_

v-'at

1993 NASA Aerospace Battery Workshop -793- Advanced Technologies Session

Page 20: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

gT,

b')

1993 NASA Aerospace Battery Workshop -794- Advanced Technologies Session

Page 21: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

Xiim

x...

m

m

m

!1_0

I

1993 NASA Aerospace Battery Workshop -795- Advanced Technologies Session

Page 22: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

SYSTEMS. INC.

OFf Ce_l Test Matrix (75 Cells)

TEMPERATURE

PROFILE

HOT

ACTION

PERFORMED

100%

DISCHARGE

TRANSI'ENT }

DISCHARGE

DAY 6

!

2,3

GROUP NO.

DAY 30

2,3

DAY 60

2,3

DAY 90

100% 4 5 6

DISCHARGE

ROOM TRANSIENT 5,6 5,6 5;_ 6DISCHARGE

100%

DISCHARGE

8,98,9COLD8,9TRANSIENT'

DISCHARGE

.

DAY 120

9

i,

Note I :

Note 2:

means transient discharge will be perfGcmed during

105"F section of hot temperature profile.

" means transient discharge will he performed during 30"F

section of cold temperature profile.

1993 NASA Aerospace Battery Workshop -796- Advanced Technologies Session

Page 23: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

m

al m

16--

0Im

al m

Im

m

m

m

1993 NASA Aerospace Battery Workshop -797- Advanced Technologies Session

Page 24: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

III. C. CELL DEVELOPMENT TESTING

TRANSIENT PROFILE

Load

0.16A

0.5A

3.5A

0.5A

3.5A

0.7A

1.0A

2.5A

5.0A

8.0A

10.0A

15.0A

30.0A

Totals

Duration

I0 Minutes

20 Minutes

250 Milliseconds

15 Minutes

250 Milliseconds

15 Minutes

5 Minutes

5 Minutes

5 Minutes2 Millisecond

3 Minutes

3 Minutes

3 Minutes

84 Minutes

AH Consumption

0.0267 AH

0.1667 AH

0.0002 AH

0.1250 AH

0.0002 AH

0.1750 AH

0.0833 AH

0.2083 AH

0.4167 AH

0.0000 AH

0.5000 AH

0.7500 AH

1.5000 AH

3.9521 AH

1993 NASA Aerospace Battery Workshop -798- Advanced Technologies Session

Page 25: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1993NASAAerospaceBatteryWorkshop -799- Advanced Technologies Session

Page 26: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

m

im

m

0

>

•"_ 0>, _ ,_0 _ ._oZ"0 m (9

Ilm

0 0 0Z Z Z

dZ

if)

W

1993 NASA Aerospace Battery . Workshop

m

-800- Advanced Technologies Sessiono

Page 27: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

X|m

x...

m

m

1993 NASA Aerospace Battery Workshop -801- Advanced Techn.ologies Session

Page 28: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

SYSTEMS. INC.

RSS Cell Test Matrix

TEMPERATURE

PROFILE

HOT

ROOM

COLD

ACTION

PERFORMED

100%

DISCHARGE

TRANSIENT _

DISCHARGE

100%

DISCHARGE

TRANSIENT

DISCHARGE

100%

DISCHARGE

DAY 6 DAY 30

2,3

5,6

GROUP NUMBER

Note i:

Note 2:

TRANSIENT'

DISCHARGE 8,9

DAY 60 DAY 90 DAY 120

2 3

2,3 2,3 3

5 6

5,6 5,6 6

8 9

8,9 8,9 9----u--

means transient discharge will be performed during IIS"F section

of hot temperature profile.

' means transient discharge will be performed during 30"F section

of cold temperature profile.

1993 NASA Aerospace Battery Workshop -802- Advanced Technologies Sessio.

Page 29: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0I

IlI

0L.

0

0III

t_L.

I

I

1993 NASA Aerospace Battery Workshop .-803- Advanced Technologies Session

Page 30: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I o C. CELL DEVELOPMENT TESTING

TRANSIENT PROFILE

Load

0.10A

3.65A

0.10A

8.00A

0.10A

0.50A

3.65A

0.50A

8.00A

0.50A

1.00A

3.65A

1.00A

8.00A

1.00A

Duration

i0 Minutes

250 Milliseconds

i0 Minutes

2 Milliseconds

i0 Minutes

8 Minutes

250 Milliseconds

8 Minutes

2 Milliseconds

8 Minutes

5 Minutes

250 Milliseconds

5 Minutes

2 Milliseconds

5 Minutes

69 Minutes

AH

0.0166

0.0002

0.0166

0.0000

0.0166

0.0666

0.0002

0.0666

0.0000

0.0666

0.0833

0.0002

0.0833

0.0000

0.0833

0. 500

1993 NASA Aerospace Battery Workshop -804- Advanced Technologies Session

Page 31: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

i

1993 ArYl_ Aerospace Battery Workshop -805- Advanced Technologies Session

Page 32: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I. C. RSS CELL DEVELOPMENT TESTING

CAPACITIES vs. TIME

HOT TEMPERATURE CHARGED STAND

DAY 90 18.4

18.2

19.0

18.5

18.7

14.4"

17.7

19.6

20.4

20.0

AVERAGE !_ - .5. 18.2 * 20.0 _8_ S +_.4.9 ....

2 61_8"9 ±

DAY 120 ...............................19.3 __ __8_..__-........19.0

18.4

19.6

18.5

_u_,-_ 19.o

19.2

17.6

18.1

18.7

18.3

18.4

18.4

18.9

18.1

19.6

19.3

19.3

18.9 18.8 +-

1.7

1993 NASA Aerospace Battery Workshop -806- Advanced Technologies Session

Page 33: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I. C. RSS CELL DEVELOPMENT TESTING

CAPACITIES vs. TIME

COLD TEMPERATURE CHARGED STAND

_,z . _-- z,, ._:'a a'_:;,::::".'.'.=""_........ = m ,_.aa = _ z = ,_am=z= =zn=am_T._-.'_= =:_..zaa .-#.:m===_a:n:z._:_n.._"-_.._==:=_=.'-.==.==:am;_::=:.'_.:::."_:=_._n==..-_._"_=.=_-_:_.-_T_:._-_._-_..=='_-_:_:==_;:_:_=_;==::=:::z-

OR IENTAT ION

DAY OF DISCHARGEUPRIGHT -UP +POS

INITIAL 20.8 20.8 21.8 21.2 + 1.7

DAY 90 19.5

20.6

20.2

19.9

AVERAGE 20.1

20.9 20.9

21.2

21.0 20.9................................ p ....................................................................

20.8 21.0 20.6 ± 1.6

_DAL!20..........................................................?A'_°_......................................_L-4.................................20:0........................................................

21.0 22.0 22.3

21.5 22.1 22.3

.............................................................................2.1._,..s_............................21._7.............................._.22-1 .......................................................22.0 21.9 21.5

21.2.......................................................... e ...................................................................... _ ................................................................

AVERAGE 21.4 22.0 21.6 21.7 ± 1.9__-_-_ .-.:=:=:-_:::=. _-==.,m m:___ = a:a::.'::...-_,,.:a _::= = =:.':::;.'::::a-.'z _,,::_:::a:_ a :; ::,'.'a,_,_ = =:= _ _:a = _ = :_ _: = ............... ==a_ :_;:a =;:z,_::= =a-'m,-: ::::= a=:::." :::=':,-'_,= r_: :: a ;:::=aa ;:_ _;:::: ::= ;=:::_:=: ;..-=.=::=_-a=_a=a:=a_ := ::::::=,,-'.'a:: .-,._,'v:'.,.a-_,-':'a=_--:',a ::::n;:: _.-.' a =::::=:::._:: ::-::::',:

1993 NASA Aerospace Battery Workshop -807- Advanced Technologies Session

Page 34: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I. C. RSS CELL DEVELOPMENT TESTING

CAPACITIES vs TIME

ROOM TEMPERATURE CHARGED STAND

ORIENTATION

DAY OF DISCHARGEUPRIGHT -UP +UP

...............................

INITIAL 23.0 22.3 22.3 22.5 ± 1.2

DAY 90 21.9

21.4

AVERAGE 21.7

DAY 120 19.7

20.2

AVERAGE 20.0

22.5 21.4

22.5 21.4 21.8 -+ 1.5

20.0 19.4

19.7 20.1

20.5 . . ..............................

20.1 20.0 20.0 -+ I.i

1993 NASA Aerospace Battery Workshop -808- Advanced Technologies Session

Page 35: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

iim

--_ >

4) _er.- 01

4) 0> ,-0 .c.

0 4)

cn -_

0 0Z Z

1993 erospace Battery Workshop -809- Advanced Technologies Session

Page 36: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

I993 NASA Aerospace Battery Workshop -810- Advanced Technologies Session

Page 37: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1993 AerospaceBatteryWorkshop -811- Advanced Technologies Session

Page 38: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

es es es i_. es es

0

W>,,

I:1

II

¢0t_el_

¢0

ilm

¢0

est_¢0

es

<<<< =

I:: t[_,_ 0 0_'00 0 0 0 0 0= 3: rr rr _

rnmmmMmrn_3 r_ r_ r_ C3 C3

1993 NASA Aerospace Battery Workshop -812- Advanced Technologies Session

Page 39: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

01m

--. m

>0 _

00 s.

Wm

m

t_ --0 0Z Z

s._Z30

..CCO

s._0

>,I

/

"0

O'J"--

._ 0m m

m

F_ _E m _,

0 CzO _

1993 NASA Aerospace Battery Workshop -813- Advanced Technologies Session

Page 40: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

"0

1993 NASA Aerospace Battery Workshop -814- Advanced Technologies Session

Page 41: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

z

1993 NASA Aerospace Battery Workshop -815- Advanced Technologies Session

Page 42: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

W

CI

0

iim

0t_

0

'r' -r "_ -r" _ -r

E E E• -, ,., 0 0 "_ "0oooo_

I-- "r" "r rr rr" 0 0

I_ u.u.u.u.u.u.

dz

nn

1993 NASA Aerospace Battery Workshop -816- Advanced Technologies Session

Page 43: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

U

IXm

IL0

¢1)

t_

m

m

>0 _'JO 00 "-

0 m

m

c6

m

m

Cmm

E!.._

0 0 0ZZZ

1993 NASA Aerospace Battery Workshop -817- Advanced Technologies Session

Page 44: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0

II lllll

¢/1m

.C er'"0 ¢0 ¢0

1993 NASA Aerospace Battery Workshop -818- Advanced Technologies Session

Page 45: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

NO'I?.:_ _ SN_*/N

_IO"LT.: ks sb_rn _'_r _nv£.."_r_m.xr.al _,*wr.._-:c/.

FIGURE I

1993 NASA Aerospace Battery Workshop41%

Advanced Technologies Session

Page 46: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

J

SYSTEMS, INC.

RSS VIBRATION

The order of testing shall be Y Axis, then X Axis, followed by theZ Axis.

The Cold Profile is to be vibrated at the following levels:

RANDOM VIBRATION CRITERIA (90 seconds in each axis)

RADIAL AXIS (Y Axis)

20-200 Hz @ 0.02 g2/Hz

200-250 Hz @ +9.4 d_/oct250-800 Hz @ 0.04 gL/Hz

800-2000 Hz @ -7.6 dB_oct2000 Hz @ 0.004 g_/Hz

LONG. AND TANG. AXES (Z and X

respectively)

20 Hz @ 0.02 g2/Hz

20-100 Hz @ +5 dB/oct100-800 Hz @ 0.3 g_Hz

800-2000 Hz @ -ii dB_oct2000 Hz @ 0.01 g_Hz

Composite = 6.6 grms Composite = 17.4 grms

The Hot Profile Unit is to be vibrated at the following levels:

Reentry Random Vibration (90 seconds in each axis)

RADIAL AXIS (Y Axis)

20 - i00 Hz @ 0.05 g2/Hz

i00 - 200 Hz @ +6.0 _B/oct200 - 500 Hz @ 0.2 g_Hz

500 - 2,000 Hz @ -5.0 d_/oct2,000 Hz @ 0.02 g_Hz

LONG. AND TANG. AXES (Z and X

respectively)

20 Hz @ 0.01 g2/Hz

20 - i00 Hz @ +8.2g_dB/oct_8_/Hzi00 - 4OO Hz @ 0

400 - 2,000 Hz @ -6.1 d_/oct2,000 Hz @ 0.03 gL/Hz

Composite = 12.9 g[_s Composite = 22.6 gr_

1993 NASA Aerospace Battery Workshop -820- Advanced Technologies Session

Page 47: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

SYSTEMS, INC.

RSS ORDNANCE SHOCK Ref. Doc. 10SPC-0225 Para. 3.2.7.2.2.1

The order of testing shaft be X+, X-, Y+, Y-, Z+, Z-.

50 Hz @ 12 G's peak50-100 Hz @ +12 dB/oct

100 Hz @ _7 C's peak100-_000 Hz @ +6 dB/oct

_000-10000 Hz @ 1,875 G's peak

RSS WATER IMPACT SHOCK Ref. Doc. 10SPC-0225 Para. 3.2.7.2.2.2

The order of testing shall be X+, X-, Y+, Y-, Z÷, Z-.

Water Impact (1 shock per axis per mission for all axes)

Longitudinat Axis and Lateral Axes

20 Hz @ 50 C's peak

20-70 Hz @ +8 dB/oct

70-5000 Hz @ 250 C's peak

1993 NASA Aerospace Battery Workshop -821- Advanced Technologies Session

Page 48: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

FIGURE I

1993 NASA Aerospace Battery Workshop -822- Advanced Technologies Session

Page 49: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

SYSTEMS, INC.

OFI VIBRATION

The order of testing shall be Z Axis, then Y Axis, followed by theX Axis.

The Cold Profile Unit is to be vibrated at the following levels:

RANDOM VIBRATION CRITERIA (90 seconds in each axis)

RADIAL AXIS (Z Axis) -

120 seconds

20 Hz @ 0.050 g2/Hz

20-48 Hz @ +3 dB/pct

48-750 Hz @ 0.12 gZ/Hz

750-2000 Hz @ -9 dB/oct2000 Hz @ 0.0064 g_Hz

Composite = 11.2 grms

LONG. AND TANG. AXES (X and Y

respectively) - 90 seconds

20 Hz @ 0.02 g2/Hz

20-100 Hz @ +5 dB/oct

100-800 Hz @ 0.3 g_/Hz

800-2000 Hz @ -ii dB_oct2000 Hz @ 0.01 g'/Hz

Composite = 17.4 grms

The Hot Profile Unit (Paragraph 4) is to be vibrated at the

following levels:

Reentry Random Vibration (90 seconds in each axis)

RADIAL AXIS (Z Axis)

20 - i00 Hz @ 0.05 g2/Hz

i00 - 200 Hz @ +6.0 _B/oct200 - 500 Hz @ 0.2 g_Hz

500 - 2,000 Hz @ -5.0 d_/oct

2,000 Hz @ 0.02 g_Hz

Composite = 12.9 grls

LONG. AND TANG. AXES (X and Y

respectively)

20

i00

400

20 Hz @ 0.01 g2/Hz

i00 HZ @ +8.2 _B/oct400 Hz @ 0.8 g'/Hz

2,000., @-6.1 d /oct2,000 Hz @ 0.03 gL/Hz

Composite = 22.6 gr=

1993 NASA Aerospace Battery Workshop -823- Advanced T¢chnoloBiea Session

Page 50: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

SYSTEMS. INC.

The order of testing shaIt be Z+, Z-, Y+, Y-, X+, X-.

OFI ORDNANCE SHOCK Ref. Doc. 10SPC-0226 Para. 3.2.7.2.2.1

50 Hz @ 12 G's peak

50-100 Hz @ +12 dB/octI00 Hz @ 47 G's peak100-4000 Hz @ +6 dB/oct

4000-10000 Hz @ 1,875 G's peak

• OFI Water Impact (l shock per axis per mission for all axes)

20 Hz @ 50 C's peak

20-70 Hz @ +8 dB/oct70-5000 Hz @ 250 G's peak

1993 NASA Aerospace BatterY Workshop -824- Advanced Technologies Session

Page 51: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

L.mm

• • • • • •

1993 NASA Aerospace Battery Workshop -825- Advanced Technologies Session

Page 52: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1993 NASA Aerospace Battery Workshop -826- Advanced Technologies Session

Page 53: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

0iim

.QL_

mm

1993 NASA Aerospace Battery Workshop -827- Ad_,anced Technologies Session

Page 54: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

iim

miim

t_

/

> ¢1)iim

m--- t_•,-, I::.C

m

m

D 0

0 mE

CL_

Em

,)20

s.. G) 4..r"0 0G)

¢1) Q-'< _ Camll

"Q 0 "- (1)I',- L_:_W C >,.Q U)t/)C .,., 0

2 o

W_

1993 NASA Aerospace Battery Workshop -828- Advanced Technologies Session

Page 55: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

iim

(D

0iim

Wl

m

"0G)C0

em

0C=3

0mD.

m

m

s_

4)0

C

4)0

"13

_. > ._,•-- 0(a OL_ L_

L. t_W C 0

"oo .c "om v) o

¢_ o ._m

ff)_'O--

im

1993 NASA Aerospace Battery Workshop -829- Advanced Technologies Session ...

Page 56: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

"5_ "6

e-

.0

• _.=.o__=

_,_ o o_:_ _

•5_ ___-_ _ _

Advanced Technologies Session1993 NASA Aerospace Battery Workshop -830-

Page 57: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

1

0

1993 NASA Aerospace Battery Workshop -831- Advanced Technologies Session

Page 58: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:
Page 59: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

List of Attendees

Loc Adamedes

BST Systems78 Plainfield Pike Road

Plainfield. CT 06374

(203) 56.1-4078

Peggy N. AdamsU.S. Army Space & Strategic Defense CommandPOB [500

Attn: CSSD-SD-AM

Huntsville, AL 35807-3801

(205) 955-1599

Menahem Anderman. Ph.D.

ACME-Advanced Energy Systems528 West 21st Street

Suite 6

Tempe, AZ 85282

(602) 894-(>864

David Baer

Hughes Aircraft Company

MS 231/1518

Electron Dynamics Division

POB 2999

Torrance, CA 90509-2999

(310) 517-7604

Bob Bechtel

Marshall Space Flight CenterEBTI

Marshall Space Flight Center, AL 35812

(205) 544-3294

Charles W. Bennett

Martin Marietta Astro Sl_aceMS NP-2I

POB 800

Princeton, NJ 08543.0800

(609) 951-7597

Tom Berry

TRW GRO / FOT

Go0dard Space Flight Center

Code 5195, Bldg. 14, P.m. E2T2Greenbelt. MD 20770

(301) 286-4184

Sam BognerHughes Aircraft company1275 New York Dr.

Altadena, CA 91001

Yannick Borthomieu

SAFT Advanced Batteries

Rue G. Leclanche

BP 1029

86060 Poitiers Cedex

France

(33) 49554014

Jeff Brewer

Marshall Space Hight CenterEB74

Marshall Space Flight center, AL 35812(205) 544-3345

Harry BrownNaval Surface Warfare Center - Crane Div.

Commander

Code 6095 B2949

300 H_/301

Crane, IN 47522

(812) 854-1593

David Burns

Marshall Space Flight CenterEB15

Marshall Space Flight center, AL 35812

(205) 544-4807

Joseph A. Carcone

Sanyo Energy (USA) Corporation

2001 Sanyo Avenue

San Diego, CA 92173(619) 661-45620

Franco Carnevale

lnmarsat

c/o Martin Marietta Astro Space

MS 115, POB 800Princeton, NJ 08543

(609) 490.6249

John E Casey

Lockheed Engineering & Sciences Co.2400 NASA Rd. 1, EP5

Houston, TX 77058-3799

(713) 4834)446

Guy ChagnonSAFI" R&D Center107 Beaver Ct.

Cockeys_lle, MD 21030

(410) 771-3200

Lee C'hristensen

Freudenberg Nonwovens20 Industrial Ave.

Chelmsford, MA 01824

(508) 256-6588

Mark Christopher

Physitron, Inc.3304 Westmill Dr.

Huntsville, AL 35805

(205) 5344844

Dwaine Coates Anne conley Eric C. Dare,/"

Eagle Picher Industries, Inc. Hughes Aircraft Johnson Space Centert215 West B St. 10345 Mary Ave. MS EP6

Joplin, MO 64802 Cupertino, CA 95014 NASA Rd. 1(417) 623.8000 X403 (408) 744-1927 Houston, TX 77058

(713) 483-9055

:_6CEt)tN_ PAL_E BLANK NOT FILMED

1993 NASA Aerospace Battery Workshop -833-

Page 60: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

/

Stephen F. Dawson

J¢¢ Propulsion Laboratory4800 Oak Grove Dr.

Pasadena, CA 9]]09

(818) 354-4329

Frank Deligiannis

Jet Propulsion LaboratoryMS 277-104

,1800 Oak Grove Dr.

Pasadena, CA 91109

(SIS) 354-04O4

Dan Dell

Gates Aerospace BatteriesPOB 147115

Gaincs-ville, FL 32614-7115

(904) 462-6914

Sal DiStcfano

Jet Propulsion LaboratoryMS 277.212

4800 Oak Grove Drive

Pasadena, CA 91109

(818) 354-6320

Rajiv Doreswamy

Marshal{ Space Flight CenterEB73

Marshall Space Flight Center, AL 35812

(205) 544-3366

Orville O, Dunham, Jr.

Ribbon Technology Corp.POB 30758

Gahanna, OH 43230

(800) S4S-0477

Andrew F.Dunnct[NTEI.SAT

MS 33A

3400 International Dr. NW

Washington, DC 20008

(202) 944-7245

Martin W. Earl

COMSAT Laboratories

22300 Comsat Dr.

ClaAsburg, MD 20871

(301) 428-4503

Frank Echols

Teledyne BrownMS 52

300 Sparkman Dr.Huntsville, AL 35807

Tim A. Edgar

Eagle Picher Industries, Inc.

3820 South Hancock Expressway

Colorado Springs, CO 80911(719) 392-4266

Ted Edge

Marshall Space Flight CenterEB11

Marshall Space Flight Center, AL 35812(205)544-3381

RobertEdgin_onNational-Standard24101 N. Home St.

Mishawaka, IN 46545

Blake A. Emmerich

Zircar Products, IncPOB 458

II0 N. Main St.

Florida, NY 10921-0458

(914) 651-4481 X2_"x)

Ted Enomoto

Sanyo Energy (USA) Corporation2001 San_3 Avenue

San Diego, CA 92173(619) 661-6620

Ed Rtzgerald

Teledync Brown F._gineeringMS 16

300 Sparkman Dr. N'W

Huntsville, AL 35807

(2O5) 726-2865

Nicanor A. Flordeliza

GE American Communications

4 Research WayPrinceton, NJ 08540

(609) 987-4453

Chris Fox

Eagle-Picher Industries, Inc.1215 West B Siree!

Joplin, MO(417) 623-8000 X367

Garry Freeman, Jr.

U.S. Army Space & Strategic Defense CommandRoute 1, Box 246

Somerville, AL 35670

(205) 955-45'76

Chris Garner

Naval Research LaboratoryCode 8134

4555 Overlook Ave. SW

Washington, DC 20375

(202) 767-9075

Dr. William O. Gentry, P.E.Johnson Controls, Inc,POB 591

Milwaukee, WI 53201

(414) 228-2228

John Gilmer

Eagie-Picher Industries, Inc.C and Porter Streets

Joplin, MO 64801

1993 NASA Aerospace Battery Workshop -834- "

Page 61: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

Eugena Goggans

Marshall Space Flight CenterEBI5

Marshall Space Flight Center,AL 35812

(205)544-3386

Ray GoinsUSBI2926 Bethel Rd.

Toney, AL 35773(205) 423-6902

Robert S. Green

Hughes - HITC

1768 Business Ctr. Dr.

Rcston, VA 22090

(703) 759-1244

Shahid Habib

NASA HeadquartersCode OW

Washington,DC 20546

(202)358-0536

Charles Hall

,Marshall Space Flight CenterEB74

Marshall Space Flight Center, AL 35812(205) 544-3330

David Hall

MarshallSpace FlightCenterEB72

Marshall Space Flight Cemer, AL 35812(2O5) 544-4215

Steve Hall

Naval Surface Warfare Center - Crane Div.

Code 6095

Crane, IN 47522

(812) 85,4-1593

Gerald Hall_rt

Jet Propulsion LaboratoryMS 277-212

4800 Oak Grove Drive

Pasadena, CA 91109

(818) 354-5474

Dr. Alan C Harkness

Ballard Battery Systems Corporation1164 West 15th St.

North Vancouver, B.C,Canada VTP IM9

(6O4)9_.4104

James R. Henderson

Westinghouse Electric Corp.

917 Explorer BoulevardHuntsville, AL 35806

(205)971-4710

Carole A. Hill

The Aerospace CorporationMANZ/2_POB 9045

Albuquerque, N,'M 87119-9045

(505) 846-7063

A/ben Himy

W_tiaghous¢ Electric CorporationPOB 18249

Pittsburgh, PA 15236(412) 382-7883

Elmer Hughett

The Enser CorporationPOB 18728

Huntsville, AL 35804-8728

John lvcrson

Aero Quality6101 NW 198 Terr.

Miami, FL 33015

(305)624-2435

Loma Jackson

Marshall Space Flight CenterEB72

Marshall Space Flight Center, AL 35812

(205) 544-3318

1L Roy Jackson

The Easer CorporationPOB 18728

HuntsviUe,AL 35804-8728

Doris Jallice

Goddard Space Flight CenterCode 734.5

Greenbelt, MD .7M/71

Jason F. Jenkins

Johns Hopkins University / APLRm 23-21.4

Johns Hopkins Rd.Laurel, MD 20723-6099

(301.)953-5106

Dr. Chris Johnson

Boeing Defense & SpaceMS 8C-61

POB 3999

S_attle, WA 98124

(206) 773-99.57

Mark Kauchak

Westinghouse

917 Explorer Blvd.Huntsville, At. 35806

(205) 971.4704

Marcie Kennedy

Marshall Space Flight CenterEB72

Marshall Space Flight Center, AL 35812(2O5)544.3724

1993 NASA Aerospace Battery Workshop -835-:

Page 62: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

Lt. VJctona KennedyU.S. Air Force

PL/V'IVC

Kinland AF'B, I_ 871i7-60_

(SOS)846-2637

Donald Kieis

It0 Wynn Drive

Huntsville,AL

Michael D. Koellmg

Hughes AircraftMS CHSS

16800E, C,entreTech ParkwayAurora,CO 80011

(303) 341-3327

AI Kuehl

USASSDC

Active Sensors Division

CSSD-SD-AMPOB 1500

Hums'vile, AL 35807-_01

Hiroaki Kusawake

National Space Development Agency of JapanTsukuba Space Center

2+1 Sengen_ Tsukuba. [barald 305Japan

81-298-52-2285

AllanLamb

19672-286Stuens Creek Blvd.

Cepertino,CA 95014

(408)282.2040

Roy Lanier

Marshall Space Flight Center

EBTI

Marshall Space Flight Center, AL 35812(205) 5_-330]

Ron LantzyMartin MariettaMS $4017

POB 179

Denver, CO 80201

(303) 971-8706

Christine Lehr

Martin Marietta Astro SpacePOB 8_

Princeton, NJ 08543-0800

(609)490-3574

Harlan L. Lewis

Naval Surface Warfare Center - Crane Div.

Crane, IN 47522-5060

(s12) _4-4104

Herman G. Lewis, Jr.

McDonnell Douglas Aerospace

MS B3.D420/22-25301'BoisaAve.

Huntington Beach, CA _'2.647

(714)896-3137

Karl Ligsin

Marshall Space FlightCenter

EB15

Marshall -Space .Flight Center, AL 35812

EricLower/

Marshall Space Flight centerEB74

Marshall Space Flight Center, AL 35812(205) 544-0080

Steve Luna

Marshall Space Flight CenterEB72

Marshall Space Flight Center, AL 35812

(205) 544-3402

Chuck Lurie

TRW

MS R4/1082

One Space ParkRedondo Beach, CA 90278

(310)813-4888

Michael Mackowski

McDonnell Douglas

7714 Asagom Ct.Hanover, MD 21076

(410) 519-0017

Dr. TylerX. Mahy

U.S.Government

e/o OTS-2S83, NHB

Washington, DC 205{)5

(7O3) 8744)739

Michelle Ma nT.o

Lewis I_rch Center

MS 309-1

21_ Brook-park Rd.Cleveland, OH 44135

(216) 433-$261

Nehemiah Margalit

Tmcor Battery Technology Center4294 Mainsail Dr.

Burke, VA 22015

(30Z)25Z-488Z

Dean W. Mau_r

AT&T ] BellLabs

379 Princeton-Hightstowngd.

Cranbu W, NJ (_$12

(609)448-0687

Louis C Maus

Marshall Space FlightCenterPDI4

Marshall Space FlightCenter, AL 35812

(205)544-0484

-1...9..9...3.NASA AerospaceBattery Workshop -836-.-..

Page 63: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

Kurt McCatl

Xl_halt Space Flight CenterEBI2

Marshall Space Flight Center, AL 35812

(205) 961-4501

Win. Keith McCoy

Sandia National LabsPOB 5800

MS 0980 Dept. 9231Albuquerque,_ 87185-0980

(505)844-7170

David D. McGuire

Martin Marietta

9390 S. Warhawk Rd.

Conifer, CO 80433

(303) 977-8647

Carol McQueary

Hughes Aircraft

Electron Dynamics DivisionPOB 15999

Torrance. CA 90509

John Metcalfe

CAL Corporation

Engineeringand QualityGroup1050Morrison Drive

Ottawa, Ontario

Canada K2H 8K7

(613) 820-8280

George Methlie

2120 Natahoa Ct.

Falls Church, VA 22043

(202) 965-3420

John Meyer

Johns Hopkins University / APL

Bldg 23/205

Johns Hopkins Rd.Laurel. MD 2072_3-6099

(301) 953-50O0 X8604

Joc,cph F. Mibelli

JFM Engineering, Inc.7880 NW 56th St.

Miami, FL 33166

(305) 592-2272

Ron Miller

Goddard Space Flight Center

Code 405, Bldg. 12, Rm. E-8Greenbelt, MD 20771

(301) 286-.6331

Scott D. Miller

Martin Marietta - UARS FOT

Code 506.9; Bldg. 3, Rm. S-24

Goddard Space Flight CenterGreenbelt, MD 20771

(301)286-3854

Zan¢ Miller

Sandia National Labs

POB 5800

MS 0980 Dept. 9231

Albuquerque, NM 871854)980

(505) 844-1426

Arnold Mondrow

BoeingPOB 440272

Aurora, CO 80044-0272

(303) 77n-707a

Bruce Moore

Naval surface Warfare Center - Crane Div.Code 6095

300Hwy 361

Crane,IN 47522

(812) 854-1593

Kensuke Nakatani

Sanyo Electric Co., Ltd.221-I Kaminaizen, Sumoto, Hyogo

Japan

(0n-_1)799-23-2851

Suzannc Norris

Martin Marietta

MS $4017

POB 179

Denver,CO 80201

(303)971-8807

Pat O'Donnell

Lewis Research CenterMS 309-1

21000 Brookpark Rd.Cleveland, OH 44135

(216) 433-5248

William Todd Owens

Auburn University

231 Leach ScienceCenter

Space Power InstituteAuburn, AL 36849-3501

(2O5) 844-5141

Craig Patio

Hughes Aircraft Co.

Colorado Engineering Laboratory

16800 E. CentreTech ParkwayAurora, CO 80017

(303) 766-9492

Gene Pearlman

Martin Marietta Astro SpacePOB 800

Princeton, NJ 08540

(609) 490-3349

Catherine Pcnafiel

Loral Aerosys7375 Executive Place

Scabrook, MD 20706

(301) 286-9316

Nguyet H. Phan

The Aerospace Corporation

M/S M2/275POB 92957

Los Angeles,CA 90009-2957

(310)336-2295

1993 NASA Aerospace Battery Workshop -83%.%....: - .

Page 64: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

David F Picke¢t

tlughes Aircraft Co.

Electron Dynamics Division

MS 231/1040POB 2999

Torrance. CA 90509-2999

(310) 517-7501

Agnes-Marie PonehusSAF'F Advanced Batteries

Rue G. Leclanche

BP 1029

86060 Poitiers Cedex

France

Dana L. Potter

Hughes Aircra[tMS CHSS

16800 E. CentreTech ParkwayAurora, CO 80011

(303) 341-3327

R. Ramesham

Auburn UniversitySpace Power Institute231 Leach Center

Auburn, AL 36849-3501

(205)844.5894

Gopal Rao

Goddard Space Flight CenterCode 734_5

Grcenbeh. MD 20716

(301) 286-6654

PhilipG. Russell

Yardney TechnicalProducts

82 Mechanic St.

Pawcatuck,CT 06379

(2O3)599-1100

B. Rutkauskas

MDESC

Upper HuttonSt. Charles, MO 63303

David K Schmidt

Gates Aerospace BatteriesPOB 147115

Gainesvilie, FL 32614-7115

(90_) 462-6947

Jack Schmidt

GE American Communications

95 Edsall Dr.

Sussex, _ 07461

(609) 987-4356

Todd Schutt

Marshall Space Flight CenterEBI2

Marshall Space Flight Center, AL 35812

(205)544-2027

Darren Stoles

F._gie-PicherIndustries,Inc.

3820 South Hancock F_,x,pressway

Colorado Springs,CO 80911

(719)392-4266

Ramakrishnan Sermadcvi

Inmarsa[

c/o Martin Marietta Astro SpaceMS 115, POB 80O

Princeton, NJ ¢_.s43

(609) 490-6301

James A. SteproNational Standard Co.

2401 N. Home St.

Mishawaka, IN 46545

(219) 259-85O5

Jo¢ Stockel

Office of Research & Development

Ames Building, Rm 762

Washington, DC 20505

(703) 351-2065

Benjamin TauschMartin Marietta

MS $40i7

POB 179

Denver, CO 80201

(3O3) 971-8"/06

Lawrence Thaller

The Aerospace CorporationMS M2/275POB 92957

Los Angeles, CA 90009

(310) 336-5180

H. E. Thierfelder

21 Dechen Rd.

Conshohocken, PA 19428

(215) 828-5765

Mark R. Toil

McDonnell Douglas Electronic SystemsMS 50O 4174

POB 426

St.Charles,MO 63301

(314)925-7692

Greta Tracinski

Applied Power International

[236 N Columbus Ave., #41Glendale. CA 91202-1672

(818) 243-3t27

Walter A. Tracinski

Applied Power International1236 N. Columbus Ave., Suite 41

Glendale, CA 91202-1672

(818) 243-3127

Jean Vernioll¢

European Space AgencyESTEC/X]'BPOB 299

2200 AG NoordwijkThe Netherlands

31-17198-3868

1993 NA.SA Aerospace Battery Workshop -838-

Page 65: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

| [a rl_, Wanncmacher

McDonnell Douglas

7404 Executive Place

Seabrook, MD 20706-O001

(331) 464-3331

Marvin Warshay

Lewis Research Center

MS 301-5

21000 Brookpark Rd.

Cleveland, OH 44135

(216) 433-5261

William Wells

Viem Corpora6on

Suite 825

400 Virginia Ave SW

Washington, DC 20024

(202) 646..6350

James IL Wheeler

Eagle-Picher Industries, Inc.

POB 47

Joplin, MO 64801

(417) 623-8000 X359

Tom Whirr

Marshall Space Flight Center

EB72

Marshall Space Right Center, AL 35812

(205) 544-3313

Don Williams

Marshall Space Flight Center

PD14

Marshall Space Right Center, AL 35812

Glenn Zeideis

DSTI

600 Blvd. S., Ste. 301

Huntsville, AL

(205) 4669233

I

...4o.,CU m

1.40

U a.a.,._ _'_

U tU I_u

• I_X

• ,._ 0 0,.--4 _ 0

Ill0m

g

,i-i

I

,IJ

I

Ill

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U _-_._ _._

• ,4 VI 4../

.,.4 0 0•--4 _ U

0ul

I

.,.4

Page 66: N94-28136 - NASA...SYSTEMS, INC. OFI VIBRATION The order of testing shall be Z Axis, then Y Axis, followed by the X Axis. The Cold Profile Unit is to be vibrated at the following levels:

f

Form Approved

REPORT DOCUMENTATION PAGE o.s _o o7o4-olse

Public reporting burden for this collection of information is est=mated to average 1 hour Der response, including the time for revlewln@ instruc_ionsc search=rig existing data sources,gathering and mamta.nmg the data needed, and completing and rev.ewlng the collection of _nformation &end comments recjard_ng thas burden estimate or any other asDect of th=s

collection of information, including suggestions for reducing this burden to Washington Headquarters Services. Oire_orate tor bnforrnatton OperatiOns and Reports, 1215 JeffersOn

Dav*s Highway, Suite 1204, Arlington. VA 22202-4302, and to the Office of Management and Budget. Paperwork Reduction Pro ect (0704-01B8). WashingtOn, DC 20503.=

1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3, REPORT TYPE AND DATES COVERED

February 1994 Conference Publication!4. TITLE AND SUBTITLE 5. FUNDING NUMBERS

The 1993 NASA Aerospace Battery Workshop

LG. AUTHOR(S)

Jeffrey C. Brewer, Compiler

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

George C. Marshall Space Flight Center

Marshall Space Flight Center, Alabama

9. SPONSORING/ MONITORINGAGENCYNAME(S)AND ADDRESS(ES)

National Aeronautics and Space Administration

Washington, DC 20546

8. PERFORMING ORGANIZATIONREPORT NUMBER

M-739

10. SPONSORING/MONITORINGAGENCY REPORT NUMBER

NASA CF-3254

11. SUPPLEMENTARYNOTESProceedings of workshop sponsored by the NASA Aerospace Flight Battery Systems

Program, hosted by the Marshall Space Flight Center, and held at the U.S. Spaceand Rocket Center on November 16-18, 1993.

12a. DIST'RIBUTION / AVAILABILITY STATEMENI:

Unclassified-Unlimited

Subject Category: 44

12b. DISTRIBUTION CODE

13. ABSTRACT (Maximum 200 words)

This document contains the proceedings of the 26th annual NASA Aerospace Battery

Workshop, hosted by the Marshall Space Flight Center on November 16-18, 1993. the

workshop was attended by scientists and engineers from various agencies of the

U.S. Government, aerospace contractors, and battery manufacturers, as well asinternational participation in like kind from a number of countries around theworld.

The subjects covered included nickel-cadmium, nickel-hydrogen, nickel-metal

hydride, and lithium based technologies, as well as advanced technologies

including various bipolar designs.

14. SUBJECTTERMS battery, nickel-cadmium, nickel-hydrogen,

nickel-metal hydride, lithium, cadmium, battery test,

electrode, pressure vessel, charge control

.,...

17. SECURITY CLASSIFICATIONOF REPORT

Unclassified

NSN 7S40-01-280-5500

18. SECURITY CLASSIFICATION 19. SECURITY CLASSIFICATION

OF THIS PAGE OF ABSTRACT

Unclassified Unclassified

*U. S. GOVERNMENT P_NTiNG OFFICE :1994-535-141

15. NUMBER OF PAGES

85116. PRICE CODE

A99i 20. LIMITATION OF ABSTRACT

LTLStand=ardForrn 298 (Rev 2-89)Prescribed _ AN&I cJtd Z]9-tS-

298- v02

Zi

.i