model cessna 182

7/21/2019 Model Cessna 182

http://slidepdf.com/reader/full/model-cessna-182 1/471

Armand J. Chaput

4900 re!stone "ri#e

Austin$ %e&as '8'31

SAVE( so)t*are is intended )or educationa+ purposes on+!. %he cop!*riteho+der grants users permission to ma,e copies )or un+imited use ut users sha++cite cop!right ho+der )or a++ deri#ati#e #ersions$ app+ications and uses inc+udingpu+ications. o responsii+it! ia accepted )or app+ications to actua+ air s!stemdesign.

a/chaputmai+.ute&as.edu

222014 - asseom input Sre) and initia+ span ca+cu+ation are redundant - +oo

Armand ! Chaput

hange record

at ho* to est comine ase+ine inputs *ith trade stud! parametric #aria+es

9 Basic SAVE Input Descriptions

Atmospheric conditions

y Field barometric pressure [in-H!"

y #emp abo$e std% day[De&!"

Field ele$ation [H'-(ft!"

Air $ehicle definition and scalin

Desin )a*imum +in ,oadin lbm.s/ft0

&on$ered ma*imum 1in loadin lbm.s/ft0

)inimum mission 2s fps0

Startin baseline 1in reference area Sref-s/ft0

Starting "a#eline overall vehicle $etted area ratio - S$et%Sre& (nd)

Converged S$et%Sre&

+in Aspect 3atio A3 - nd0

+in #aper 3atio #3 - nd0

+in ,E S1eep [derees!"

4ominal 1in thic5ness.chord ratio t.c - nd0

'ing S$et%Splan ratio

'inglet plan&orm area &raction - "oth #ide# (S$nglt%Sre& - nd)

Vertical tail plan&orm area &raction (Svt%Sre& - nd) - #tarting value

'inglet and empennage S$et%Splan ratio

'inglet a!c! location (Cmac &raction - nd)

Si'in options" 6 7 Fi*ed eom8 input +af .S

ref : 7 Fi*ed eom8calc +

ref ; 7

Fi*ed fuse.nac.pod8 si'ed 1in and tails8 calc +af .Sref < 7 Si'ed fuse.nac.pod81in and tails8 calc +af .S

ref8 = 7 Scaled parametric eometry8 input +

2o1er-to-1eiht ratio BHp> .+

>8 hp.lbm0

BHp> .+

> re/?d to meet ta5eoff nd roll at con$ered +>.Sref

Startin baseline fuselae@nacelle@pod 1etted area S1et fnp - s/ft0

u#elage S*et

S*et-)use

- s)t5

acelle S*et

S*et-nac

- s)t5

*od S*et

S*et-pod

- s)t5

Starting +, $ing epo#ed plan&orm area &raction (S*e&pSre) - nd5

.ori/ontal tail plan&orm area &raction (Sht%Sre& - nd) - #tartingvalue

Vertical ail Volume Coecient (VVC - nd)

ther 1in and tail definition not re/?d for ;6(0

+> desin static marin fraction of &mac0"

+in &mac leadin ede FS0

Hori'ontal tail Cmoment armC ft0

Vertical tail Cmoment armC ft0

$erall air $ehicle mass properties

Enine or )otor 2o1er-to-+eiht 3atio BHp>.+en0 [BHp.lbm!"

Enine or )otor installation 1eiht factor +en-inst.+en0"

4ose ear 1eiht fraction +nl.+>0"

)ain ear 1eiht fraction +ml.+>0"

Empty 1eiht ro1th marin fraction +e1m.+e0

2arametric airframe 1eiht multiplier

Input airframe unit 1eiht +af.Sref psf0

Fuselae@nacelle@pod 1eiht per unit S1et 1fnp - psf0

+in 1eiht per unit e*posed planform area 11 - psf0

Empennae 1eiht per unit planform area 1fnp - psf0

&on$ered B+

End of mission fuel lbm0

Airframe 1t

Air $ehicle component $olume

.ori/ontal ail Volume Coecient (,ht%Cmac)(Sht%S

re& ) (.VC - nd)

+in Aerodynamic &enter fraction of &mac

4eutral 2oint ,ocation fraction of &mac)3

Fi*ed baseline desin +> options 6-;0 or initial +

> estimate options <8 =0 [lbm!"

Design maximum retained installed internal payload 1eiht [lbm!"

Design maximum retained installed e*ternal payload 1eiht [lbm!"Design maximum e*pendable internal payload 1eiht [lbm!"

Design maximum e*pendable e*ternal payload 1eiht [lbm!"

Design maximum fuel or battery 1eiht fraction +f.+>0"

Systems@a$ionics 1eiht fraction +spa

)isc% +eiht Fraction +misc

.seful,oad0"

2arametric airframe 1eiht +af .S

ref7 >%:9 +

ref >%<

&on$ered +> .S

&on$ered +af .S

,andin fuel reser$e fraction +f land

.+f desin ma*

Volume marin fraction re/?d

Fuselae usable $olume fraction

2od usable $olume fraction

4acelle usable $olume fraction

+in usable $olume fraction

Fuselae ross $olume a$ailable cuft0 - as dra1n

4acelle ross $olume a$ailable cuft0 - as dra1n

2od ross $olume a$ailable cuft0 - as dra1n

+in ross $olume a$ailable cuft0 - as dra1n

%ota+ usa+e #o+ume a#ai+a+etota+ #o+ume re6d

Air $ehicle component densities

Internal retained payload density8 installed lbm.cuft0

E*ternal retained payload density8 installed lbm.cuft0

Internal e*pended payload density8 installed lbm.cuft0

Fuel or battery0 density8 installed lbm.cuft0

Enine or motor0 density8 installed lbm.cuft0

Systems@A$ionics +eiht density8 installed lbm.cuft0"

4ose ear density8 installed lbm.cuft0

)ain ear density8 installed lbm.cuft0

)isc% +eiht density8 installed lbm.cuft0

+eiht ro1th marin density8 installed lbm.cuft0

Body eometry re/uired for dra build-up aero assessment

7od +ength )t5 - i) integrated *ith another od!$ enter th )or oth

Aero-SG& definition

ace++e #o+ume re6d a#ai+ : VS;n nd5

;use+age < pod #o+ume re6d a#ai+ : VS;)p nd5

E*ternal e*pended payload density8 installed lbm.cuft0

;use+age +ength )t5 - i) integrated *ith another od!$ enter th )oroth

;use+age =neness ratio ;> : )"e)5 - i) integrated *ith nace++e$enter ;> )or oth

ace++e +ength )t5 - i) integrated *ith another od!$ enter th )oroth

ace++e =neness ratio ;> : n"en5 - i) integrated *ith anotherod!$ enter ;> )or oth

7od =neness ratio ;> : p"ep5 - i) integrated *ith nace++e$ enter;> )or oth

#a5eoff ,ift &oefficient &,8t.o

&,8stall

- In Fliht8 4o Flaps

&,8stall

- In Fliht8 Flaps

,andin ,ift &oefficient &,8land

Airfoil ma*imum thic5ness location chord fraction0

ther Dra D./ psf0"

3etained payload D./ psf0

E*pended payload D./ psf0

s1ald Efficiency"

4ominal fuselae-nacelle-pod installed interference dra factor

4ominal fuselae-nacelle-pod laminar fraction

4ominal 1in-1inlet-tail installed interference dra factor

4ominal 1in-1inlet-tail laminar fraction

2ropulsion definition

Enine #ype BE 7 68 I&7 :0"3eference speed for static thrust calculation appro* >% Vt.o - (#AS0

Fi*ed Eta2 option 6 7 constant $alue8 > 7 calculated $alue0

Fi*ed Eta2

2ropeller desin speed 5ts0

Desin propeller efficiency"

Variable pitch prop .40

For BE2rop enter battery enery [+h.lbm!"

For BE2rop enter nominal motor efficiency Eta)0

For I&2rop enter SF&> lbm-hr-Bhp0For #urbochared I&2rop enter flat rate altitude (ft - enter >%> for no #&0

I&2rop installed po1er fraction of uninstalled0

I&2rop Secondary Shaft 2o1er #a5eoff [+!"

I&2rop mi*ture ratio for round operations

I&2rop mi*ture ratio for ta5eoff8 climb and landin

I&2rop mi*ture ratio for reduced po1er fliht sements

End of mission CfuelC residual lbm0

)inimum mission 2s fps0

)ission definition and performance re/uirements

y #a5eoff and landin speed marin"

y )inimum in Fliht speed marin

Initial estimate of o$erall e/ui$alent S5in Friction &oefficient &fe0

)ission a$erae 3eynolds number adusted e/ui$alent s5in friction coefficient&fe0

&D> multiplier - (dra for use later for model calibration0"

#rim Dra - Fraction of &D8i

#hrust multiplier - (t used later for model calibration0"

Mission required fraction of desin ma*imum retained internal payload

Mission required fraction of desin ma*imum retained e*ternal payload

Mission required fraction of desin ma*imum e*pendable internal payload

Mission required fraction of desin ma*imum e*pendable e*ternal payload

Mission required fraction of desin ma*imum fuel

y Enine start and system chec5 time min0

Enine start and system chec5 throttle settin fraction0

y #a*i out time min0

#a*i out throttle settin fraction0

#a5eoff time min0

y #a5eoff Distance [ft!"

#2 re/?d cur$e fit0

#2 a$ail calculated0

y #a5eoff and climb throttle settin fraction0

Desired rotation and ta5eoff speed (&AS0

)in allo1able ta5eoff speed (&AS0

Desired &limb Speed [(&AS!"

)in allo1able climb speed [(&AS!"

&ruise altitude )S, (ft0

&ruise distance nm0

Initial climb @ accel distance nm0

Desired &ruise Speed [(#AS!"

Desired &ruise Speed [(&AS!"

)in allo1able cruise speed [(#AS!"

Search altitude )S, (ft0

Search altitude A, (ft0

)a* search altitude for detection A, (ft0

)a* search altitude for ID A, (ft0

,e$el fliht search time min0

)in re/?d le$el fliht search time for detection min0

)in re/?d le$el fliht search time for ID min0#urnin fliht search time min0

)in re/?d turnin fliht search time for detection min0

#otal search time min0

Steady state search turn ban5 anle de0

)in re/?d search ban5 anle for detection de0

)in re/?d search ban5 anle for ID de0

Desired 1ins le$el search speed [(#AS!"

Desired 1ins le$el search speed [(&AS!"

)in allo1able search speed [(#AS!"

Desired search turn speed [(&AS!"

)in allo1able search turn speed [(&AS!"

Sur$eillance altitude )S, (ft0

Search altitude A, (ft0

)in re/?d sur$eillance slant rane for detection (ft0

)in re/?d sur$eillance slant rane for ID (ft0

Sur$eillance time min0

Steady state sur$eillance ban5 anle de0

)in re/?d sur$eillance ban5 anle for detection de0

)in re/?d sur$eillance ban5 anle for reconition de0

)in re/?d sur$eillance ban5 anle for ID de0

Desired Sur$eillance Speed [(&AS!"

)in allo1able sur$eillance speed [(&AS!"

Ependa"le payload drop option (1 drop 0 retain)

E*pendable payload drop altitude )S, (ft0

E*pendable payload drop speed (&AS0

E*pendable payload drop time min0

,andin loiter altitude (ft0

,andin loiter time min0

4ominal landin loiter ban5 anle de0

Desired landin loiter speed [(&AS!"

)in allo1able landin loiter speed [(&AS!"

,andin time min0

y ,andin throttle settin fraction0

#a*i bac5 time min0

,andin CfuelC reser$e fraction0

End of mission CfuelC residual lbm0

#otal mission time min0

Fliht time ta5eoff to land0

#aret definition

y #aret search area 1idth nm0

y #aret search area lenth nm0y #aret search area ele$ation (ft )S,0

y #aret orientation h 7 hori'ontal8 $ 7 $ertical0

y Search taret si'e m0

Estimated search reconition s1ath 1idth 5ft0

Estimated search time to turn ;> de min0

&alculated search time to turn ;> de based on input ban5 anle min0

y Sur$eillance taret si'e m0

Estimated sur$eillance reconition $ie1in radius 5ft0

Estimated sur$eillance time to turn ;> de min0

&alculated sur$eillance time to turn ;> de based on input ban5 anle min0

ther Inputs 4ot re/?d for ASE ;6(0

)otor and 2rop Inputs not ready for ASE ;6 use0

Battery $oltae E E0

Electronic speed controller ES&0 amp ratin A0

ption to calculate BE2rop motor efficiency Eta)0 .40

)otor speed coefficient ($ 32).V0

)otor resistance 3m ms0

)otor idle corrent slope I.E A.V0

ther sensor payload definitions - not on Sp:>6: list

Sensor payload definitions - basic

3e/?d sensor 2i*els on #aret 2o#0 - detection

3e/?d sensor 2i*els on #aret 2o#0 - reconition

3e/?d sensor 2i*els on #aret 2o#0 - identification

Search sensor $ie1in anle de0

)a* allo1able search $ie1in anle de0

Sur$eillance sensor $ie1in anle de0

)a* allo1able sur$eillance $ie1in anle de0Search s1ath o$erlap factor decimal J7 6%>0

Search sensor field of $ie1 de0

Sur$eillance sensor field of $ie1 de0

Sensor focal plane array si'e )pi*0

Sensor colors or contrast le$els per pi*el

Sensor $ideo frame rate frames.s0

sable sensor search detection s1ath 1idth (ft0

sable sensor search ID s1ath 1idth (ft0

$erall payload definitions - not on Sp:>6: list

Sensor uninstalled 1eiht +sen - lbm0

Sensor payload installed 1eiht factor +sen-inst.+sen0"

Sensor uninstalled po1er 2sen - +0

Sensor payload installed po1er factor 2sen-inst.2sen0"

Sensor payload uninstalled density 3ho-sen - pcf0"

Sensor payload installed density factor 3ho sen-inst.3ho sen0"

)otor idle corrent intercept I> A0

Sensor payload dra area D./ sen - s/ft0"

ther payload definition retained - internal0

ther payload retained-internal0 1eiht +oprein-lbm0"

ther payload retained-internal0 1eiht install% factor +oprein-inst.+oprein0"

ther payload retained-internal0 installed po1er 2oprein - +0"

ther payload installed po1er factor 2oprein-inst.2oprein0"

ther payload retained-internal0 uninstalled density 3ho oprein - pcf0"

ther payload retained-internal0 density factor 3ho oprein - inst.3ho oprein0"

ther payload retained-internal0 dra area D./ oprein - s/ft0"

ther payload definition retained - e*ternal0

ther payload retained-e*ternal0 1eiht +opree*-lbm0"

ther payload retained-e*t%0 1eiht install% factor +opree*-inst.+opree*0"

ther payload retained-e*ternal0 installed po1er 2opree* - +0"

ther payload retained-e*ternal0 dra area D./ opree* - s/ft0"

ther payload definition e*pended - internal0

ther payload e*pended-internal0 1eiht +op*pin-lbm0"

ther payload e*pended-int% 1eiht installation factor +op*pin-inst.+op*pin0"

ther payload e*pended-internal0 installed po1er 2op*pin - +0"

ther payload e*pended-internal0 uninstalled density 3ho op*pin - pcf0"

ther payload definition e*pended - e*ternal0

ther payload e*pended-internal0 1eiht +op*pe*-lbm0"

ther payload e*pended-internal0 installed po1er 2op*pe* - +0"

ther payload e*pended-e*ternal0 dra area D./ op*pe* - s/ft0"

System si'e and cost

round turn around time minutes0

2ropulsion mass fraction distribution

op*pin0"

ther payload e*pended-internal0 1eiht install% factor +op*pe*-inst.+op*pe*0"

;raction o) insta++ed propu+sion +ocated in od! re)erenced nace++e?1 decima+5

;raction o) insta++ed propu+sion +ocated in od! re)erenced nace++e?2 decima+5

;raction o) insta++ed propu+sion *ing mounted in 1<>1 nace++esdecima+5

+in referenced mass fraction distribution

Fraction of retained internal payload located in.on 1in decimal0

Fraction of retained e*ternal payload located in.on 1in decimal0

Fraction of e*pended internal payload located in.on 1in decimal0

Fraction of e*pended e*ternal payload located in.on 1in decimal0

Fraction of fuel or battery located in 1in decimal0

Fraction of systems@a$ionics located in 1in decimal0

Fraction of nose ear located in.on 1in decimal0

Fraction of main ear located in.on 1in decimal0

Fraction of empty 1eiht marin located in.on 1in decimal0

Fraction of misc% 1eiht located in.on 1in decimal0

Empennae referenced mass fraction distribution

Fraction of systems @ a$ionics in.on hori'ontal tail decimal0

Fraction of systems @ a$ionics in.on $ertical tail decimal0

Fraction of systems @ a$ionics in.on 1inlets decimal0

Body referenced component locations FS0

3etained internal payload located in.on body FS0

E*pended internal payload located in.on body FS0

E*pended internal payload located in.on body FS0Fuel or battery located in.on body FS0

Body referenced enine or motor K6 FS0

Body referenced mounted enine or motor K: FS0

Systems@a$ionics located in.on body FS0

4ose ear located in.on body FS0

)ain ear located in.on body FS0

Empty 1eiht ro1th marin located in.on body FS0

)isc% 1eiht located in.on body FS0

Fuselae c%% FS0

Body referenced nacelle 6 c%% FS0Body referenced nacelle : c%% FS0

Body referenced pod c%% FS0

+in referenced component locations FS0

3etained internal payload located in.on 1in &mac fraction0

3etained e*ternal payload located in.on 1in &mac fraction0

E*pended internal payload located in.on 1in &mac fraction0

;raction o) insta++ed propu+sion *ing mounted in 2<>2 nace++esdecima+5

E*pended e*ternal payload located in.on 1in &mac fraction0

Fuel or battery located in 1in &mac fraction0

+in mounted ,6@36 enines or motors &mac fraction0

+in mounted ,:@3: enines or motors &mac fraction0

Systems@a$ionics located in 1in &mac fraction0

4ose ear located in.on 1in &mac fraction0

)ain ear located in.on 1in &mac fraction0

Empty 1eiht ro1th marin located in.on 1in &mac fraction0

)isc% 1eiht located in.on 1in &mac fraction0

4acelle ,6.36 located in.on 1in &mac fraction0

4acelle ,:.3: located in.on 1in &mac fraction0

+in pounted pod c%% &mac fraction0

+in c%%&mac fraction0

Enine.motor nacelle locations FS0

S*et )raction o) pod re)erenced to *ing S*et-*podS*et-pod5

od! re)erenced nace++e 1 )raction o) nace++e S*et S*et-nac1S*et-nac5

od! re)erenced nace++e 2 )raction o) nace++e S*et S*et-nac2S*et-nac5

@ing mounted nace++e 1<>1 )raction o) nace++e S*et S*et-nac1<>1S*et-nac5

@ing mounted nace++e 2<>2 )raction o) nace++e S*et S*et-nac2<>2S*et-nac5

Decision rationale or reference

:9%: :>66 lo1 O15

:%6 :>66 hih O15

>%>> (ED& s

;%;6L 6G:" con$ered 1in loadin8 ;" 5ept same until 1in test O15

>%66 Bhp>" motor data sheet8 +>" mass measurements O15

>%>LL=

;%L;> measured on rtf model O15

<%=6L measured on rtf model O15

%9; measured on rtf model O2

=%9>; measured on rtf model O15

>%9 measured on rtf model O15

>%>> 4o pods O15

%L>: &alculated from measurement data O15

>%L E/ui$alent trape'oidal 1in calculation O15

< E/ui$alent trape'oidal 1in calculation O15

>%6=>6: E/ui$alent trape'oidal 1in calculation O15

>%9>< measured on rtf model O15

:%;< measured on rtf model O3

>%>> 4o 1inlets O15

>%:;9 measured on rtf model O2

>%69 measured on rtf model O2

>%<6 measured on rtf model O3

>%>>> 4o +inlets O3

Air Vehicle5e#ign

>%<L &alculated from measurement data O3

>%> &alculated from measurement data O3

>%:=> #ypical airfoil 361L

>%;> Estimate 361L

>%6= 3e/uirement 361L

>%L VS2 361L

:%6 VS2 O3

:%<= VS2 O3

6:%<= mass measurements s

>%>>> rtf" no payload8 bl" mass measurements s

>%6=> rtf" no payload8 bl" mass measurements s>%=>> rtf" no payload8 bl" mass measurements s

>%>>> rtf" no payload8 bl" mass measurements s

>%6>> mass measurements s

:%L> Bhp>" motor data sheet8 +en" mass measurements s

6%::> mass measurements s

>%;< mass measurements s

>%>> mass measurements s

>%>:= mass measurements s

>%>>> Estimate s

>%6>>Estimate

1.0646 Estimate s

>%9;9 mass measurements s

>%<9;mass measurements

>%<; mass measurements s

>%>=< mass measurements s

0.747 s

>%L>> Estimate s

>%>>> 4o pods s

6%>>> definition s

>%=>> Estimate s

>%6; VS2 &ompeom s

>%6;> VS2 &ompeom s

>%>>> 4o pods s

>%>>> no storae in 1ins s

6<% Estimate s

6%>E@> definition s

6> &D Estimate s6%>E@> definition s

6=%> &D Estimate s

;%>> Estimate s

=%>> &D Estimate s

6%>E@> definition s

:=%> &D Estimate s

;%6>measured on rtf model

<%;&alculated from measurement data

>%<measured on rtf model

>%>&alculated from measurement data

>%>> 4o pods s

>%>>4o pods

6%;= Estimate M 1ill $erify 1ith *flr= s

6%: Estimate M 1ill $erify 1ith *flr s

6%: no flaps s

6%;= Same as ta5eoff s

=%>> H+ s

0.15 H+= s

;%>> H+ s

>%6= H+= s

>%6> H+ s

69L H+ s

;6%> )anufacturer D &

:=%=> )anufacturer &alc

6%> H+ s

:=%> H+ s

6%>> H+6 s

>%:= H+ s

;>%> H+ s

6%>>> H+6 s

>%<> s

6=%>> H+ s

>%96=%>> H+ s

:>%>> s

;>%> H+ s

;=%>> H+ s

6%>>> H+6 s

>%<> )anufacturer (f s

5.00 H+ s

30 H+ s

;>%>> H+ s

6 H+ s

6 H+6 s

;> H+ s

6% H+ s

>%L> H+6 s

6%>> H+ s

6= H+ s

;:%> H+ s

6%> H+ s

>%6= H+ s

:%> H+ s

>%>> H+ Sn

>%6;> H+ Sn>%>> H+ Sn

h H+ Sn

:%>>> H+ Sn

>%6>> H+ Sn

>%:=> H+ Sn

6%>>> H+ Sn

>%>= H+ Sn

6%>>> H+ Sn

66>:%>>

6%> Sn

:>%> Sn

;=%> Sn

90.00 Sn

80.506%6> Sn

>%;<= Sn

6%>> Sn

;>%>> Sn

:6<%>>

6%>>E@>

:%>>6%>>

6L>%>>

>%>>>6%;:<

>%>>;%<9

Direct Input

Slider input

#ransfer from &ommonData

&omputational &ell

B+ lbm0

Desin BHp> hp0

#. BHp> hp0

6%< 6%<

>%=69 >%69=

6%=L :%:6

# B, )ass Factor # B, )ass Factor

0.911 2.424

Input +af .S

multiplier

)ult * +af .S

con$ered +> .S

)anned A unit 1in1t% param% For +>.Sref

tradesSailplane unit 1in 1t%

param for A3 trades

++ at con$ered+>.Sref

0 10 20

12.B20

12.B30

12.B40

12.BB0

12.B'0

12.B80

12.B90

12.'00

12.'10

12.'20

'eight C

7 r o # # ' e i g h t ( l " m )

1000.00

nd 3oll A$ail ft0

30 40 0 B0 '0

nvergence

6teration

:9%: :9%: :9%:

:%6 :%6 :%6

>%>> >%>> >%>>

6 : 6 ; :

6%<9 -6%L<9:= 6%<9 -6%L<9:=>>> 6%<9 -6%L<9:=>>6

6%< -6%L=69<;: 6%< -6%L==>9=<6: 6%< -6%L<9:=>>6

>%666>LL66 >%>>6>LL6 >%666>LL66 >%>>6>LL66 >%666>LL66 >%>>6>LL66

>%>;96 ->%><9;9;6 >%>;9> ->%><9<L>== >%>;9: ->%><9;:<L;6

;%: -<%:;=:= ;%> -<%L>>=>><:;: ;%= -<%<9>=>9<

<%>9> >%:>:L <%>9> >%:>:L <%>9> >%:>:L

;%L6= ->%>:=;L: ;%L6= ->%>:=;L: ;%L6= ->%>:=;L:

;%L6= ->%>:=;L: ;%L6= ->%>:=;L: ;%:>L -6%;6>6;:6

=%:;; -6%<>;6:= =%:;; -6%<>;6:= =%:;; -6%<>;6:=

=%:;; ->%>;6:= =%:;; ->%>;6:= =%:;; ->%>;6:=

>%>> ->%9 >%>> ->%9 >%>> ->%9

>%>> >%>> >%>>

%:L< ->%=6L><<6< %:L< ->%=6L><<6<: %:L< ->%=6L><<6<;

>%< ->%>;96<:L >%< ->%>;96<:L=6 >%< ->%>;96<:L=

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ref8 = 7 Scaled parametric eometry8 input +

2o1er-to-1eiht ratio BHp> .+

>"- BHp.lbm0

BHp> .+

> 3e/uired to )eet #a5eoff Distance"

n baseline fuselae@nacelle@pod 1etted area S1et fnp - s/ft0

;use+age S*et

S*et-)use

- s)t5

ace++e S*et

S*et-nac

- s)t5

7od S*et

S*et-pod

- s)t5

@ing %aper >atio nd5 - chec; &or #ingularity at9 1

Starting *ing e&posed p+an)orm area )ractionS

re) - nd5

@ing+et p+an)orm area )raction - oth sidesS*ng+tSre)5

Dnput hori(onta+ tai+ p+an)orm area )ractionShtSre)5

Dnput #ertica+ tai+ p+an)orm area )raction S#tSre)5 >%69

@ing+et and empennage S*etSp+an ratio >%<>L

@ing+et a.c. +ocation Cmac )raction5 >%>>>

Ca+cu+ated ase+ine *ing span - )t5 =%<

Ca+cu+ated %VC >%:L

Ca+cu+ated V%VC >%>

&on$ered eometry - basic

S1et.Sref - from eom iter <%=6L

+in 3eference Area [s/ft!" ;%L;

#otal +etted Area [s/ft!" 6=%<:

+etted Aspect 3atio" 6%9<

Fusele 1etted area s/ft0" =%9>

se+age and pod con#erged +inear sca+e )actor re6d 6%>>

4acelle 1etted area s/ft0" >%9

ace++e con#erged +inear sca+e )actor re6d 6%>>

2od 1etted area s/ft0" >%>>

E*posed 1in planform area [s/ft!" ;%<

@ing con#erged +inear sca+e )actor re6d 6%>>

Span b0 [ft!" =%<

>%L;;>%=L

+in ma* chord thic5ness s1eep de0 :%;<

+inlet planform area - both sides - s/ft0 >%>>

Hori'ontal #ail planform area [s/ft!" >%9:

Vertical tail planform area [s/ft!" >%=

Ca+cu+ated ase+ine nomina+ od! diameter at*ing od! intersection "

i - )t5

ori(onta+ %ai+ Vo+ume CoeFcient %VC5 :htCmac5S

ref 0"

Vertica+ %ai+ Vo+ume CoeFcient V%VC5 : Cmac5S

ref 0"

+in e*posed area fraction S1e*p

$erall $ehicle $olumetric efficiency Volume:.; .S1et - nd0

Fuselae@4acelle@2od +etted Area S1et-:O1in@tailplanform areas00 [s/ft!"

4ominal 1in body intersection diameter Dbi - ft0

Con#erged od! diameterspan ratio "i5

+in 3oot &hord &r [ft!"+in tip &hord &

t [ft!"

)ean Aerodynamic &hord &mac

a+ tai+ moment arm re6d )or input ShtSre) ht - )t5 :%::

a+ tai+ moment arm re6d )or input S#tSre) ht - )t5 :%<=

ShtSre) re6d )or input #t nd5 >%:<

S#tSre) re6d )or input ht nd5 >%69

ther 1in and tail definition not re/?d for ;6(0@ing Cmac +eading edge ;S5 >%L

'0 de#ign #tatic margin (&raction o& Cmac)3 >%6=

Hori'ontal tail moment arm ft0 :%6>

Vertical tail moment arm ft0 :%<<

+in ape* location - FS 0ft0 ->%6=

&mac leadin ede location - FS ft0 K3EFN

Sht.Sref re/?d to meet input H#V& at input location >%:;9

S$t.Sref re/?d to meet input V#V& at input location >%69

$erall air $ehicle mass propertiess

6:%<=>

4ose ear 1eiht fraction +nl.+>0" >%>>

)ain ear 1eiht fraction +ml.+>0" >%>:=

ear +eiht Fraction +l.+> - compare sum to 3aymer0" >%>;6

'ing Aerodynamic Center (&raction o& Cmac

eutral *oint ,ocation (&raction o& Cmac

&mac ,ocation )easured from &enterline - mac [ft!"

,E of &mac

)easured from +in Ape* - Pmac

Fi*ed baseline desin +> options 6-;0 or initial +

> estimat

options >8 <0 [lbm!"

Design maximum retained installed internal payload1eiht [lbm!"

Design maximum retained installed e*ternal payload1eiht [lbm!"

Design maximum e*pendable internal payload 1eiht[lbm!"

Design maximum e*pendable e*ternal payload 1eiht[lbm!"

Design maximum fuel or battery 1eiht fraction +f.+>0"

Enine or )otor 2o1er-to-+eiht 3atio BHp>.+en0[BHp.lbm!"

Enine or )otor Installation +eiht factor +en-inst.+en0"

Systems@a$ionics 1eiht fraction +spa

Empty 1eiht ro1th marin fraction +e1m.+e0 >%6>>

2arametric airframe unit 1eiht +af.Sref psf0 6%=;

2arametric airframe 1eiht multiplier 6%>=

Input airframe unit 1eiht +af.Sref psf0 >%9;9>

Fuselae@nacelle@pod 1eiht per unit S1et 1fnp - psf0 >%<9;

+in 1eiht per unit e*posed planform area 11 - psf0 >%<:L<L<=

)anned A unit 1in 1t% param% >%=69

Sailplane unit 1in 1t% param% >%69=

Empennae 1eiht per unit planform area 1fnp - psf0 >%>=<><99<

&on$ered B+ [+>-lbm!" 6:%>L

&on$ered ma*imum 1in loadin +>.Sref - psf0 ;%;:

Fuel or battery 1eiht [+f-lbm!" :%6

Gninsta++ed engine or motor *eight @eng +m5 >%=>

ose gear *eight @n+g - +m5 >%>

ain gear *eight @m+g - +m5 >%;6

%ota+ a+ighting gear *eight H+mI >%;L

Air)rame *eight H@a) - +mI ;%>

Empt! *eight gro*th margin @em - +m5 >%99

Empt! *eight H@e - +mI 9%9>

seful ,oad , - lbm0 :%L6

Fuselae!"a#elle!$%d &ei't (*np + l,- ;%;>

Fuselae &ei't *use + l,-) :%96

"a#elle &ei't na# + l,-) >%;9

$%d &ei't p%d + l,-) >%>>

in &ei't (& + l,- 6%<

inlet &ei't &nlt + l,-) >%>>

%ri%ntal ail &ei't ('t + l,- >%>=

erti#al ail &ei't (vt + l,- >%>;

ir*ra-e &ei't a* + l,-) =%>:

ir*ra-e &ei't *ra#ti%n a*/0) >%:L

)isc% +eiht Fraction +misc

.seful,oad0"

Systems @ a$ionics and landin ear fraction desin1eiht [ lbm!

Dnsta++ed engine or motor *eight @eng-inst

S!stems < a#ionics *eight @spa

isc. *eight H@misc

re* #al#ulated)

-pt &ei't *ra#ti%n e/0) >%L

)a* ross 1eiht c%% location FS-ft0 >%><

)a* ross 1eiht c%% location &mac fraction0

Qero fuel c%% location FS-ft0

Qero fuel c%% location &mac fraction0

4ose landin ear load fraction

)ain landin ear load fraction

Air $ehicle $olume and density

Volume marin fraction re/?d >%<

Fuselae usable $olume fraction >%L>>

2od usable $olume fraction >%>>>

4acelle usable $olume fraction 6%>>>

+in usable $olume fraction >%=>>

Fuselae ross $olume a$ailable cuft0 >%6;

4acelle ross $olume a$ailable cuft0 >%6;>

2od ross $olume a$ailable cuft0 >%>>>

+in bo* ross $olume a$ailable cuft0 >%>>>

Internal retained payload density8 installed lbm.cuft0 6=

E*ternal retained payload density8 installed lbm.cuft0 6%E@>

Internal e*pended payload density8 installed lbm.cuft0 6>

E*ternal e*pended payload density8 installed lbm.cuft0 6%E@>

Fuel or battery0 density8 installed lbm.cuft0 6=

Enine or motor0 density8 installed lbm.cuft0 ;%>>

Systems@A$ionics +eiht density8 installed lbm.cuft0" =

4ose ear density8 installed lbm.cuft0 6%E@>

)ain ear density8 installed lbm.cuft0 6%E@>

)isc% +eiht density8 installed lbm.cuft0 :=

+eiht ro1th marin density8 installed lbm.cuft0 :=

Con#erged gross )use+age #o+ume a#ai+a+e cu)t5 >%6

Con#erged gross nace++e #o+ume a#ai+a+e cu)t5 >%6;

Con#erged gross pod #o+ume a#ai+a+e cu)t5 >%>>

Con#erged gross *ing #o+ume a#ai+a+e cu)t5 >%>>

Con#erged gross #o+ume a#ai+a+e a#ai+a+e cu)t5 >%L<

&%% and and ear loads - from enhanced SAVE not re/?dfor ASE;6(0

Con#erged usa+e #o+ume a#ai+a+e cu)t5 >%>

Con#erged #o+ume re6d cu)t5 6%>

&on$ered $olume re/?d0.Baseline usable $ol a$ail%0 :%<;

Con#erged nace++e S*et sca+e )actor 6%>>

Con#erged nace++e #o+ume sca+e )actor 6%>>

&on$ered fuselae G pod S1et scale factor 6%>>

&on$ered fuselae G pod $olume scale factor 6%>>

&on$ered 1in area scale factor 6%>>

&on$ered 1in $olume scale factor 6%>>

Gsa+e )use+age #o+ume a#ai+a+e cu)t5 >%=

Gsa+e pod #o+ume a#ai+a+e cu)t5 >%>>

Gsa+e nace++e #o+ume a#ai+a+e cu)t5 >%6;

Gsa+e *ing #o+ume a#ai+a+e cu)t5 >%>>

%ota+ usa+e #o+ume a#ai+a+e cu)t5 >%>

3etained internal payload $olume re/?d cuft0 >%>>

3etained e*ternal payload $olume re/?d cuft0 >%>>

E*pended internal payload $olume re/?d cuft0 >%>=

E*pended e*ternal payload $olume re/?d cuft0 >%>>

Fuel or battery located in.or body cuft0 >%>6

Installed propulsion $olume re/?d cuft0 >%>6

Systems@a$ionics $olume re/?d cuft0 >%L

4ose ear $olume re/?d cuft0 >%>>

)ain ear $olume re/?d cuft0 >%>>

Empty 1eiht marin $olume re/?d cuft0 >%><

)isc% 1eiht $olume re/?d cuft0 >%>>

Volume marin re/?d cuft0 >%;

%ota+ #o+ume re6d cu)t5 6%>

@ing #o+ume a#ai+ used cu)t5 >%>>

%ota+ usa+e #o+ume a#ai+a+etota+ #o+ume re6d >%<6

- i) integrated *ith another od!$ enter th )or oth ;%6

)"e)5 - i) integrated *ith nace++e$ enter ;> )or oth <%;

- i) integrated *ith another od!$ enter th )or oth >%<=L

"ep5 - i) integrated *ith nace++e$ enter ;> )or oth >%=9

ace++e #o+ume re6d a#ai+ : VS;n nd5

;use+age < pod #o+ume re6d a#ai+ : VS;)p nd5

Body eometry re/uired for dra build-up aeroassessment

- i) integrated *ith another od!$ enter th )or oth >%>>>

"ep5 - i) integrated *ith nace++e$ enter ;> )or oth >%>>>

Aero-SG&

6%:6%:

Airfoil ma*imum thic5ness location chord fraction0 >%;

>%>><<

ther Dra D./ psf0" >%>><

3etained payload D./ psf0 >%>>>>

E*pended payload D./ psf0 >%>><>

s1ald Efficiency" >%L=

inal fuselae-nacelle-pod installed interference dra factor 6%6>

4ominal fuselae-nacelle-pod laminar fraction >%:>

4ominal 1in-1inlet-tail installed interference dra factor 6%6>

4ominal 1in-1inlet-tail laminar fraction >%<>

ndu#ed ra Fa#t%r :) 0.048

6:%6 6:%6

)ission ,oad Factor"

,ift 3e/uired 7 +eiht * ,oad Factor"

)ission defined turn rate de.s0

)ission defined turn radius (ft0#ime to turn ;> de min0

#a5eoff8 stall or landin speed (&AS-5ts0

#a5eoff ,ift &oefficient &,8t.o

&,8stall - In Fliht8 4o Flaps&

,8stall - In Fliht8 Flaps

,andin ,ift &oefficient &,8land

Initial estimate of o$erall e/ui$alent S5in Friction&oefficient &

&D> multiplier - (

dra for use later for model calibration0"

#rim Dra - Fraction of &D8i

;er% Li*t ra <%e* + d=usted :><*>S&et/Sre* ) ! /?)/Sre* )

<L *%r L/)

<L *%r Aini-u- $%&er

)ission +eiht from end of pre$ious sement 1eiht0 -[lbm!"

)a* &, t.>8 stall or land0

Speed marin limited &,

)ission Sement &L

)ission sement &,α

)ission sement α no flaps0 7 &, .&

)arin limited min speed (&AS-5ts0

)arin limited min speed (#AS-5ts0

)ission sement speed (&AS-5ts0

)ission sement speed (#AS-5ts0

Ben%lds "u-,er

Aissi%n averae Ben%lds nu-,er ad=usted <*e 0.0049

2ropulsion

Enine #ype BE 7 68 I&7 :0" 6%>>

3eference speed for static thrust calculation >% Vt.o - 5ts0 6%=>

Fi*ed Eta2 option 6 7 constant $alue8 > 7 calculated $alue0 >%>>

Fi*ed Eta2 >%>

2ropeller desin speed 5ts0 ;L%>>

Desin propeller efficiency" >%L>

Variable pitch prop .40 n

For BE2rop enter battery enery [+h.lbm!" %=>

BE2rop electric motor efficiency Eta20 >%L=

I&2rop SF&> lbm-hr-Bhp0 6%6>

#urbochared I&2rop flat rate altitude (ft - >%> for no #&0 >%>>

I&2rop installed po1er fraction of uninstalled0 >%9>

I&2rop secondary 2o1er #a5eoff [2#-+!" >%>>

I&2rop mi*ture ratio for round operations 6%:=

I&2rop mi*ture ratio for ta5eoff8 climb and landin 6%<>

I&2rop mi*ture ratio for reduced po1er fliht sements 6%>>

<Ctri-

La-inar <*

ur,ulent <*

#hrust multiplier - (t 1ill be used later for model

calibration0"

BHp> 6%<>

SF&> 6;%69

2spto Hp0 >%>>

#hrottle settin > 7 not defined8 6%> 7 ma* po1er0 6%>> >%6=

6 6%>>

Installed po1er a$ailable [BHp!" 6%<> 6%<>

Eta-prop >%= >%=

)a* thrust a$ailable lbf0 6<%= 6<%=

Fuel flo1 at ma* a$ailable po1er lbm.hr0 6L%<< 6L%<<

Fuel flo1 re/?d to meet 2S2# re/uirement +dotFp0 >%>> >%>>

#SF& lbm.hr-lbf0 6%: 6%:

#ime 1eihted a$erae Eta-prop 0.'91

)ission definition and performance

6%>>#a5eoff and landin speed marin" 6%>>

)inimum in Fliht speed marin 6%:=

Enine start and system chec5 time min0 =%>>

Enine start and system chec5 throttle settin fraction0 >%6=

#a*i out time min0 ;%>>

#a*i throttle settin fraction0 >%6=

#a5eoff time min0 >%6>

#a5eoff Distance [ft!" 69%

#2 re/?d 31.7

#2 a$ail 25.5

#a5eoff and climb throttle settin fraction0 6%>>

Desired rotation and ta5eoff speed (&AS0 :=%>>

Desired &limb Speed [(&AS!" :=%>>

&ruise altitude )S, (ft0 6%>>

&ruise distance nm00 >%:=

Desired &ruise Speed [(#AS!" ;>%>>

For I& 2rop enter mi*ture ratio 6%> 7 mi*ture for besteconomy0

Mission required fraction of desin ma*imum retainedinternal payload

Mission required fraction of desin ma*imum retainede*ternal payload

Mission required fraction of desin ma*imum e*pendableinternal payload

Mission required fraction of desin ma*imum e*pendablee*ternal payload

Mission required fraction of desin ma*imum fuel

Desired search altitude )S, (ft0 6%>>

,e$el fliht search time min0 6=%>>

#urnin fliht search time min0 =%>>

#otal search time min0 :>%>>

4ominal search ban5 anle de0 ;>%>>

Desired 1ins le$el search speed [(#AS!" ;=%>>Desired search turn speed [(&AS!" ;=%>>

Desired sur$eillance altitude )S, (ft0 6%>>

Sur$eillance time min0 =%>>

4ominal sur$eillance ban5 anle de0 ;>%>>

Desired Sur$eillance Speed [(&AS!" ;>%>>

E*pendable payload drop altitude (ft0 6%>>

E*pendable payload drop speed (&AS0 ;>%>>

E*pendable payload drop time min0 6%,andin loiter altitude (ft0 >%L>

,andin loiter time min0 6%>>

4ominal landin loiter ban5 anle de0 6=%>>

Desired landin loiter speed [(&AS!" ;:%>>

,andin time min0 6%>>

,andin throttle settin fraction0 >%6=

#a*i bac5 time min0 :%>>

)ission ross 1eiht lbm0 6:%6

)ission retained payload 1eiht lbm0 >%6=)ission e*pended payload 1eiht lbm0 >%=>

)ission fuel 1eiht lbm0 :%6

)ission Sement Inputs"

eometric altitude )S, H'-(ft!" >%> >%>

Delta #ime [min!" =%>>

Delta Distance [nm!

Desired &AS [5ts!"

Desired (#AS [5ts!"

)inimum Allo1able (&AS"

3e/uired (&AS"

3e/uired (#AS"

Input throttle Settin fraction8 > if un5no1n0" 6%>> >%6=

Ban5 Anle [derees!"

,oad factor 4'0"

4umber of #urns"

Ependa"le payload drop option (1 drop 0 retain)

&alculations Based on #ime to &limb or Accelerate

nput %r #al#ulated t'r%ttle settin *ra#ti%n) >%6=

Se-ent t'rust availa,le l,*) 6<%=

Se-ent $s availa,le *ps)Se-ent d%tF (l,-/'r :%

Startin sement 1eiht lbm0 6:%6 6:%6

Startin sement fuel lbm0 :%6 6%9;

&limb and accel calculations &alculations

Se-ent Fli't $at' ##elerati%n F$) (Ds

i-e t% <li-, %r ##elerate (s

Distance to climb or accelerate nm0

Breuet 3ane or Endurance &alculations

Segment distance nm5Segment time min5

%hrott+e setting re6d )raction5

>ange )actor nm5

Endurance )actor

reguet )ue+ re6d +m5

%ime and distance )ue+ re6d

Elapsed #ime [min!" >%>>> =%>>>

Elapsed Distance [nm!" >%>>> >%>>>

)Ission Summary

A$erae &ruise outbound and inbound0 &," >%L6

A$erae &ruise ,.D" 6<%<;

A$erae &ruise CFuelC Flo1 [lbm.hour!" 6%<

A$erae &ruise 3ane Factor [nm!" :L<%<>

A$erae 1ins le$el search speed (#AS0 ;%;>

A$erae turnin search speed (#AS0 <>%>L

A$erae sur$eillance speed (#AS0 <>%>L

A$erae Search and Sur$eillance includin turns0 &," >%L6A$erae Search and Sur$eillance ,.D" 6<%;>

A$erae Search and Sur$eillance CFuelC Flo1 [lbm.hour!" 6%99

A$erae Search and Sur$eillance Endurance Factor [hrs!" %>L

Sur$eillance time [min! =%>>

#otal )ission CFuelC 3e/uired [lbm!" 6%<

#otal )ission Distance Includin #a5eoff [nm!" 6L%;;

#otal )ission #ime [min!" ;9%:

Fliht distance from liftoff to landin0 - nm 6L%;>

Fliht time from liftoff to landin0 - min :9%:

Desin sur$eillance time min0 =%>>,andin fuel reser$e fraction0 >%;

End of mission fuel residual lbm0 >%>6

)in in fliht 2s fps0 <6%<9

Search-Sur$eillance Endurance Factor Efss0 - hrs %>L

+af lbm0 ;%>

+en lbm0 >%=>

+f lbm0 :%6

+pay e*p >%=>

Airframe R.lbm =>

)otor R.lbm :=>

Fuel R.lbm 6>>

Sensor R.lbm :=>

2eople R.hr :>>

4umber of people ea0

)ission time min0 <>

Assumed F33 score >%9>

Assumed desin report score >%9>Assumed search obecti$e score >%=>

Assumed sur$eillance obecti$e score >%=

Assumed A#, score >%>=

,i/uid@solid payload fraction of e*pended mass >%

Assumed deli$ery accuracy >%;>

Assumed deli$ery time min0 6>

f SE &ost Estimatin 3elationship SE &E30 7 CAV &ostC R0 =:6

E &ost Estimatin 3elationship SE &E30 7 CHead &ostC R0 L>>

Airframe fraction of SE &E3 7 CAV &ostC >%;=

)otor fraction of SE &E3 7 CAV &ostC >%:<

Fuel fraction of SE &E3 7 CAV &ostC >%<6

SE Score 7 ;>> [EFss - =0.=!.&E3 sec.R0 6%6;

Deli$ery time score >%:

Deli$ery obecti$e >%:999

S&DD scorin criteria e*ample for information only - not$erified0

Fliht performance score >%=;;;

#otal score >%

R.sec sensiti$ities

6> increase in EF 0 34.0E

6> reduction in +af 1.4E

6> reduction in +en 1.0E

6> reduction in +f 1.7E

6> reduction in mission time or number of people 6.4E

ther &ommon Data 4ot re/?d for ASE ;6(0

)otor and 2rop Inputs not ready for ASE ;6 use0

Battery $oltae E $0 6<%>>

ES& amp ratin A0 :>%>>

ption to calculate BE2rop motor efficiency Eta)0 .40 n

Enter motor speed coefficient ($ 32).$0 66>:%>>

Enter motor resistance 3m ms0 >%6<>%;

Enter motor idle corrent slope I.E A.V0 6%

Sensor payload definition

3e/?d sensor 2i*els on #aret 2o#0 - detection 6%>>

3e/?d sensor 2i*els on #aret 2o#0 - reconition :>%>>

Enter motor idle corrent intercept I> A0

3e/?d sensor 2i*els on #aret 2o#0 - identification ;=%>>

Search sensor $ie1in anle de0 9>%>>

Sur$eillance sensor $ie1in anle de0 9>%>>

Search s1ath o$erlap factor decimal J7 6%>0 6%6>

Search sensor field of $ie1 de0 69%>>Sur$eillance sensor field of $ie1 de0 69%>>

Sensor focal plane array si'e )pi*0 >%;=

Sensor colors or contrast le$els per pi*el 6%>>

Sensor $ideo frame rate frames.s0 ;>%>>

Sensor uninstalled 1eiht +sen - lbm0 >%6;

Sensor payload installed 1eiht factor +sen-inst.+sen0" 6%;>

Sensor uninstalled po1er 2sen - +0 6%L>

Sensor payload installed po1er factor 2sen-inst.2sen0" 6%>>

Sensor payload uninstalled density 3ho-sen - pcf0" :6<%>

Sensor payload dra area D./ sen - s/ft0" >%>6

#aret area and sensor calculations

Sensor binary bits.pi*el b.pi*el0 <%>

ncompressed $ideo data rate )b.s0 <6%=

Search sensor instantaneous field of $ie1 IFV - rad0 =%<E-><

Search ma*imum detection slant rane S,3ma* det - m0 :6L%

Search ma*imum reconition slant rane S,3ma* rec - m0 6<%L

Search ma*imum ID slant rane S,3ma* id - m0 99%9

Search ma*ium detection altitude Hma* det A, - (ft0 >%>

Search ma*ium reconition altitude Hma* rec A, - (ft0 >%=

Search ma*ium ID altitude Hma* id A, - (ft0 >%;:;

usable search detection s1ath 1idth +se ma*u det - (ft0 >%:6;

able search reconition s1ath 1idth +se ma*u rec - (ft0 >%6>

)a*imum usable search ID s1ath 1idth +se ma*u id - (ft0 >%>9

4umber of detection search s1aths re/?d 4Sse det - ea0 :%>

4umber of reconition search s1aths re/?d 4Sse rec - ea0 :%=

4umber of ID search s1aths re/?d 4Sse id - ea0 <%<

a*imum search detection s1ath lenth ,se ma* det - (ft0 >%:6<

*imum search reconition s1ath lenth ,se ma* rec - (ft0 >%66

)a*imum search ID s1ath lenth ,se ma* id - (ft0 >%>9L

Sensor payload installed density factor 3ho sen-inst.3hosen0"

le$el search time re/?d for detection tse 1l det min - min0 >%<:

$el search time re/?d for reconition tse 1l rec min - min0 >%=:

m 1ins le$el search time re/?d for ID tse 1l ID min - min0 >%96

sable detection frame $ie1in time sec0 ;%<

sable reconition frame $ie1in time sec0 :%

sable ID frame $ie1in time sec0 6%ompressed sinle frame detection mosaic data rate )b.s0 >%<>

pressed sinle frame reconition mosaic data rate )b.s0 >%=>9

/?d uncompressed sinle frame ID mosaic data rate )b.s0 >%L9>

Search turn radius for detection based s1aths (ft0 >%6>

Search turn radius for detection based s1aths (ft0 >%>L=

Search turn radius for detection based s1aths (ft0 >%><9

Search turn load factor for detection based s1aths ?s0 6%=;

Search turn load factor for detection based s1aths ?s0 6%

Search turn load factor for detection based s1aths ?s0 :%:

Sustained search detection turn ban5 re/?d de0 <9%6LSustained search reconition turn ban5 re/?d de0 ==%;>

Sustained search ID turn ban5 re/?d de0 L%<=

Sustained search detection turn time re/?d min0 >%<>

Sustained search reconition turn time re/?d min0 >%=>

Sustained search ID turn time re/?d min0 >%L

l detection based 1ins le$el @ search turn time re/?d min0 >%L:

econition based 1ins le$el @ search turn time re/?d min0 6%>:

#otal ID based 1ins le$el @ search turn time re/?d min0 6%9

Sur$eillance sensor instantaneous field of $ie1 IFV - rad0 =%<E-><

Sur$eillance ma*imum detection slant rane S,3ma* - m0 6>9%;

ur$eillance ma*imum reconition slant rane S,3ma* - m0 L%<

Sur$eillance ma*imum ID slant rane S,3ma* - m0 =>%>

Sur$eillance detection based turn radius 3trn det - (ft0 >%>=9

Sur$eillance reconition based turn radius 3trn det - (ft0 >%><

Sur$eillance ID based turn radius 3trn det - (ft0 >%>:

Sur$eillance detectuion based time to turn ;> de min0 >%>9

Sur$eillance reconition based time to turn ;> de min0 >%>

Sur$eillance ID based time to turn ;> de min0 >%><

ur$eillance detection based sustained turn load factor ?s0 :%6

r$eillance reconition based sustained turn load factor?s0 ;%6

Sur$eillance ID based sustained turn load factor ?s0 =%;

ce detection based sustained turn ban5 anle re/?d φ

e reconition based sustained turn ban5 anle re/?d φ de0

illance detection ID sustained turn ban5 anle re/?d φ

ction based sensor roll anle in AV coord sys - θ

det- de0

nition based sensor roll anle in AV coord sys - θ rec- de0

Sensor sur$eillance detection based imain radius (ft0 >%66L

Sensor sur$eillance reconition based imain radius (ft0 >%>9=

Sensor sur$eillance ID based imain radius (ft0 >%>=<

ther payload definition retained - internal0

ther payload retained-internal0 1eiht +oprein-lbm0" >%::

ther payload definition retained - e*ternal0

ther payload retained-e*ternal0 1eiht +opree*-lbm0" >%:>

ther payload definition e*pended - internal0

ther payload e*pended-internal0 1eiht +op*pin-lbm0" >%>>

ther payload definition e*pended - e*ternal0

ther payload e*pended-internal0 1eiht +op*pe*-lbm0" :%>>

nce ID based sensor roll anle in AV coord sys - θ id- de0

ther payload retained-internal0 1eiht installation factor+oprein-inst.+oprein0"

ther payload retained-internal0 installed po1er 2oprein -+0"

ther payload installed po1er factor 2oprein-inst.2oprein0"

ther payload retained-internal0 uninstalled density 3ho

oprein - pcf0"ther payload retained-internal0 density factor 3ho

oprein - inst.3ho oprein0"

ther payload retained-internal0 dra area D./ oprein -s/ft0"

ther payload retained-e*ternal0 1eiht installation factor+opree*-inst.+opree*0"

ther payload retained-e*ternal0 installed po1er 2opree*- +0"

ther payload retained-e*ternal0 dra area D./ opree* -s/ft0"

ther payload e*pended-internal0 1eiht installationfactor +op*pin-inst.+op*pin0"

ther payload e*pended-internal0 installed po1er2op*pin - +0"

ther payload e*pended-internal0 uninstalled density 3hoop*pin - pcf0"

ther payload e*pended-internal0 density factor 3hoop*pin - inst.3ho op*pin0"

ternal0 1eiht installation factor +op*pe*-inst.+op*pe*0" 6%>>

round turn around time minutes0 6L>%>>

2ayload R.lbm0.Air $ehicle R.lbm0 =%>>

round support cre1 re/?d persons0 =

Fliht system cre1 re/?d persons0 :

)annin ratio 6%:=

Sustained cre1 1or5 1ee5 hrs.1ee50 =%>>

4ominal labor rate R.hr0 <>%>>

)aintenance man hours.FH >%=>

Spares and e/uipment R.FH

&ommunication cost R per )b.s0

4otional fractional air $ehicles re/?d 4.53

4otional payload procurement re/?d lbm0 0.00

4otional fuel procurement re/?d lbm0 9.79

4otional airframe procurement re/?d lbm0 16.30

4otional propulsion procurement re/?d lbm0 2.26

4otional a$ionics@systems procurement re/?d lbm0 4.32

4otional propulsion landin ear procurement re/?d lbm0 1.73

4otional air $ehicle procurement mass re/?d lbm0 24.61

2ayload procured mass relati$e to B,

Airframe procured mass relati$e to B,

3elati$e procurement cost

on of retained internal payload located in.on body decimal0 1.000

n of retained e*ternal payload located in.on body decimal0 1.000

of e*pended internal payload located in.on body decimal0 1.000

of e*pended e*ternal payload located in.on body decimal0 1.000

Fraction of fuel or battery located in.on body decimal0 1.000

ther payload e*pended-internal0 installed po1er2op*pe* - +0"

ther payload e*pended-e*ternal0 dra area D./ op*pe* -s/ft0"

Body referenced mass distributions and componentlocations

Fraction of systems@a$ionics located in.on body decimal0 1.000

Fraction of nose ear located in.on body decimal0 1.000

Fraction of main ear located in.on body decimal0 1.000

Fraction of misc% 1eiht located in.on body decimal0 1.000

on of retained internal payload located in.on 1in decimal0 >%>>>

n of retained e*ternal payload located in.on 1in decimal0 >%>>>

n of e*pended internal payload located in.on 1in decimal0 >%>>>

of e*pended e*ternal payload located in.on 1in decimal0 >%>>>

Fraction of fuel or battery located in 1in decimal0 >%>>>

Fraction of systems@a$ionics located in 1in decimal0 >%>>>

Fraction of nose ear located in.on 1in decimal0 >%>>>

Fraction of main ear located in.on 1in decimal0 >%>>>

Fraction of misc% 1eiht located in.on 1in decimal0 >%>>>

;raction o) insta++ed propu+sion +ocated in od!re)erenced nace++e ?1 decima+5

;raction o) insta++ed propu+sion +ocated in od!re)erenced nace++e ?2 decima+5

Fraction of empty 1eiht marin located in.on bodydecimal0

Body referenced nacelle 6 fraction of nacelle S1et S1et-nac6.S1et-nac0

Body referenced nacelle : fraction of nacelle S1et S1et-nac:.S1et-nac0

S1et fraction of pod referenced to body S1et-n1pod.S1et-pod0

+in referenced mass distributions and componentlocations

;raction o) insta++ed propu+sion *ing mounted in1<>1 nace++es decima+5

;raction o) insta++ed propu+sion *ing mounted in2<>2 nace++es decima+5

Fraction of empty 1eiht marin located in.on 1indecimal0

+in mounted nacelle ,6@36 fraction of nacelle S1etS1et-nac,6@36.S1et-nac0

Fraction of systems @ a$ionics in.on $ertical tail decimal0 >%>>>

Fraction of systems @ a$ionics in.on 1inlets decimal0 >%>>>

3etained internal payload located in.on body FS0 >%=

E*pended internal payload located in.on body FS0 >%>>>

Fuel or battery located in.on body FS0 6%;:<

Body referenced enine or motor K6 FS0 >%>>>

Body referenced enine or motor K: FS0 ;%L:L

Systems@a$ionics located in.on body FS0 :%;L:

4ose ear located in.on body FS0 >%9<>

)ain ear located in.on body FS0 ;%;>

Empty 1eiht ro1th marin located in.on body FS0 :%:>

)isc% 1eiht located in.on body FS0 :%:>

Fuselae c%% FS0 <%LL

Body referenced nacelle 6 c%% FS0 >%>>>

Body referenced nacelle : c%% FS0 ;%<L=

Body referenced pod c%% FS0 6%L9

+in 3eferenced &omponent ,ocations FS0

+in mounted nacelle ,:@3: fraction of nacelle S1etS1et-nac,:@3:.S1et-nac0

S1et fraction of pod referenced to 1in S1et-1pod.S1et-pod0

Empennae referenced mass distributions assumed to belocated at a%c%0

Fraction of systems @ a$ionics in.on hori'ontal taildecimal0

3etained internal payload located in.on 1in &macfraction0

3etained e*ternal payload located in.on 1in &macfraction0

E*pended internal payload located in.on 1in &macfraction0

E*pended e*ternal payload located in.on 1in &macfraction0

Fuel or battery located in 1in &mac fraction0 >%>>>

+in mounted ,6@36 enines or motors &mac fraction0 >%>>>

+in mounted ,:@3: enines or motors &mac fraction0 >%>>>

Systems@a$ionics located in 1in &mac fraction0 >%>>>

4ose ear located in.on 1in &mac fraction0 >%>>>

)ain ear located in.on 1in &mac fraction0 >%>>>

)isc% 1eiht located in.on 1in &mac fraction0 >%>>>

4acelle ,6.36 located in.on 1in &mac fraction0 >%>>>

4acelle ,:.3: located in.on 1in &mac fraction0 >%>>>

+in pounted pod c%%&mac fraction0 >%>>>

+in c%%&mac fraction0 >%=>>

&omm payload definition

9e<=d 9 ,8S gra/ing angle a"ove hori/on (theta - deg) >%>>

>aimum ,ine o& Sight (,8S) di#tance &rom "a#e (nm) >%>>

&ace terminal antenna height a"ove ground (?&t - A7,) >%>>>

nstalled 1eiht +rfe - lbm0 - enter > for parametric si'in >%>>

&omm 3F uninstalled po1er 2rfe - +0 >%>>

&omm 3F electronics uninstalled density 3ho rfe- pcf0" >%>>

&omm 3F electronics density factor 3ho rfe-inst.3ho rfe0" >%>>

&omm 3F antenna 1eiht +rfa-lbm0" >%>>

Empty 1eiht ro1th marin located in.on 1in &macfraction0

a#ai+a+e cu)t5 a#ai+a+e cu)t5 a#ai+a+e cu)t5 a#ai+a+e cu)t5

cu)t5 cu)t5

&omm 3F electronics installed 1eiht factor +rfe-

inst.+rfe0"

&omm 3F antenna uninstalled po1er 2rfa - +0" >%>>

&omm 3F antenna uninstalled density 3ho rfa - pcf0" >%>>

&omm 3F antenna density factor 3ho rfa-inst.3ho opa0" >%>>

&omm 3F antenna e*posed frontal area A*c rfa - s/ft0" >%>>

Systems @ a$ionics definition

nstalled 1eiht +spa - lbm0 - enter > for parametric si'in >%>>

Systems@a$ionics installed 1eiht factor +spa-inst.+rfe0" >%>>

Systems@a$ionics po1er-to-1eiht 2spa.+spa - +.lbm0 >%>>

Systems@a$ionics uninstalled density 3ho spa- pcf0" >%>>

Systems@a$ionics density factor 3ho spa-inst.3ho rfe0" >%>>

&omm 3F antenna installed 1eiht factor +rfa-inst.+opa0"

27 27 33 46 55

(ey" ,abel

Direct Input

2AV input#ransfer to &ommonData

&omputational &ell

#a*i out #a5eoff run 3otate ,iftoff Start &limb

6 :a :b ;a ;b

>%> >%> >%> >%> >%>

6%: 6%: 6%: 6%: 6%:

>%>> >%>> >%>> >%>> >%>>

>%9=<9 >%9=<9 >%9=<9 >%9=<9 >%9=<9

6%>L99 6%>L99 6%>L99 6%>L99 6%>L99

>%L6 >%L6 >%L6 >%L6 >%L6

6%>L< 6%>L< 6%>L< 6%>L< 6%>L<

9%;9;E@>; 9%;9;E@>; 9%;9;E@>; 9%;9;E@>; 9%;9;E@>;

?CAS 9e<=d v#! Elap#ed ime (min)#u"-title

'eight Convergence#u"-title

.000 10.000 1.000 20.000 2.000 30.000 3.000 40.00

>o* 398

>o* 39

Elap#ed ime (min)

? C A S ( ; t # )

0.000 10.000 20.000 30.000 40.000 0.000

,i&t- to- 5rag 9atio v#! Elap#ed ime (m#u"-title

Elap#ed ime (min!)

, i & t - t o - 5 r

a g 9 a t i o

6:%6 6:%6 6:%6 6:%6 6:%6

1.00 1.00 1.00

12.71 12.71 12.71

0.00 0.00

0.000 0.0000.00 0.00

1.35 1.27

1.35 0.81

0.10 0.10

14.02 8.43

26.92 27.76

26.92 34.70

28.77 37.07

25.00 26.92 34.70

26.71 28.77 37.07

1.840!05

>%6= 6%>> 6%>> 6%>> 6%>>

6%>> 6%>> 6%>> 6%>> 6%>>

6%<> 6%<> 6%<> 6%<> 6%<>

>%= >%= >%; >% >%L>

6<%= 6<%= 6:%<L 66%9 9%L;

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6%: 6%: 6%<L 6%=< 6%LL

>%> >%> >%> >%> >%>

;%>> >%6>

:=%>> :=%>> :=%>>

:%6 :%6 :%6

26.92 34.70

28.77 37.07

>%6= 6%>> 6%>> 6%>> 6%>>

6%>> 6%>>

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6<%= 6<%= 6:%<L 66%9 9%L;

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6:%6 6:%6 6:%6 6:%6 6:%6

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L%>>> L%6>> L%6>> L%6>> L%6>>

>%>>> >%>>> >%>;; >%>;; >%>>>

58 54 58 57

Start Accel Start &ruise ut

;%=a ;%=b <a <b

6%>> 6%>> 6%>> 6%>>

6% 6% 6% 6%

>%<> >%<> >%<> >%<>

>%9<6> >%9<6> >%9<6> >%9<6>

6%>L: 6%>L: 6%>L: 6%>L:

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6%><9 6%><9 6%><9 6%><9

9%;=96E@>; 9%;=96E@>; 9%;=96E@>; 9%;=96E@>;

End &limb sum of allmission climbs0

End Accel to ma* input(#AS0

Vehicle 'eight v#! Elap#ed ime (min)#u"-title

0.000 10.000 20.000 30.000 40.000 A0.000

0hru#t Availa"le (l"&) and 5rag (l"&) v#! Elap#ed 0im

#u"-title

>o* 33A >o* 300

Elap#ed 0ime (min!) 0 h r u # t A v a i l a " l e ( l " & ) a n d 5 r a g ( l " & )

0.000 10.000 20.000 30.000 40.000 0.000

Elap#ed ime (min!)

V e h i c l e ' e i g h t ( l " m )

0.000 .000 10.0001.00020.0002.00030.0003.00040.00

@uel lo$@ (l"m%hr) v#! Elap#ed ime#u"-title

@ u e l l o $ @ ( l "

m % h r )

6:%6 6:%6 6:%6 6:%6

1.00 1.00 1.00 1.00

12.71 12.71 12.71 12.71

0.00 0.00 0.00 0.00

0.000 0.000 0.000 0.0000.00 0.00 0.00 0.00

1.27 1.27 1.27 1.27

0.81 0.81 0.81 0.81

0.81 0.81 0.80 0.81

0.10 0.10 0.10 0.10

8.43 8.43 8.29 8.43

27.76 27.76 27.76 27.76

34.70 34.70 34.70 34.70

37.30 37.30 37.30 37.30

34.70 34.70 35.00 34.70

37.30 37.30 37.62 37.30

0.022 0.022 0.022 0.022

0.032 0.032 0.031 0.032

0.003 0.003 0.003 0.003

0.057 0.057 0.056 0.057

0.89 0.89 0.89 0.89

14.30 14.30 14.35 14.30

1.833!05 1.833!05 1.849!05 1.833!05

0.003 0.003 0.003 0.003

0.006 0.006 0.006 0.006

6%>> 6%>> 6%>> >%>>

6%>> 6%>> 6%>> 6%>>

6%<> 6%<> 6%<> 6%<>

>%L> >%L> >%L> >%L>

9% 9% 9%L 9%

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>%>> >%>> >%>> >%>>

6%L9 6%L9 6%9> 6%L9

6%>> 6%>> 6%>> 6%>>

:=%>> :=%>> ;:%= :%96

:%L :%L ;=%>> ;>%>>

34.70 34.70 34.70 34.70

34.70 34.70 35.00 34.70

37.30 37.30 37.62 37.30

6%>> 6%>> 6%>>

61 57 61 57

End &ruise ut Start Search - #urns

a 6>b 66 6:a

6%>> 6%>> 6%>> 6%>>

6% 6% 6% 6%

>%<> >%<> >%<> >%<>

>%9<6> >%9<6> >%9<6> >%9<6>

6%>L: 6%>L: 6%>L: 6%>L:

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6%><9 6%><9 6%><9 6%><9

9%;=96E@>; 9%;=96E@>; 9%;=96E@>; 9%;=96E@>;

Start Search - ,e$elFliht

End Search - ,e$elFliht

6:%6 6:%6 6:%6 6:%6

1.00 1.00 1.00 1.15

12.71 12.71 14.67

0.00 0.00 0.00 15.72

0.000 0.000 0.000 0.2470.00 0.00 0.00 0.40

1.27 1.27 1.27

0.81 0.81 0.81

0.81 0.81 0.81 0.81

0.10 0.10 0.10 0.10

8.43 8.43 8.43 8.43

27.76 27.76 27.76 29.83

34.70 34.70 34.70 37.29

37.30 37.30 37.30 40.08

34.70 34.70 34.70 37.29

37.30 37.30 37.30 40.08

0.022 0.022 0.022 0.022

0.032 0.032 0.032 0.032

0.003 0.003 0.003 0.003

0.057 0.057 0.057 0.057

0.89 0.89 0.89 1.03

14.30 14.30 14.30 14.30

1.833!05 1.833!05 1.833!05 1.970!05

0.003 0.003 0.003 0.003

0.006 0.006 0.006 0.006

>%>> >%>> >%>> >%>>

6%>> 6%>> 6%>> 6%>>

6%<> 6%<> 6%<> 6%<>

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9% 9% 9% L%L:

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6%L9 6%L9 6%L9 :%>9

6%>> 6%>> 6%>> 6%>>

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34.70 34.70 34.70 37.29

37.30 37.30 37.30 40.08

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64 57 60 62

End Search - #urns Start Sur$eil - #urns End Sur$eil - #urns 2ayload drop

6:%=a 6:%=b 6;a 6;b

6%>> 6%>> 6%>> 6%>>

6% 6% 6% 6%

>%<> >%<> >%<> >%<>

>%9<6> >%9<6> >%9<6> >%9<6>

6%>L: 6%>L: 6%>L: 6%>L:

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6%><9 6%><9 6%><9 6%><9

9%;=96E@>; 9%;=96E@>; 9%;=96E@>; 9%;=96E@>;

6:%6 6:%6 6:%6 6:%6

1.15 1.15 1.15 1.00

14.67 12.21

15.72 15.72 15.72 0.00

0.247 0.247 0.247 0.0000.40 0.40 0.40 0.00

1.27 1.27

0.81 0.81

0.81 0.81 0.81 0.81

0.10 0.10 0.10 0.10

8.43 8.43 8.43 8.43

29.83 29.83 29.83 27.76

37.29 37.29 37.29 34.70

40.08 40.08 40.08 37.30

37.29 37.29 37.29 34.70

40.08 40.08 40.08 37.30

0.022 0.022 0.022 0.022

0.032 0.032 0.032 0.032

0.003 0.003 0.003 0.003

0.057 0.057 0.057 0.057

1.03 1.03 1.03 0.89

14.30 14.30 14.30 14.30

1.970!05 1.970!05 1.970!05 1.833!05

0.003 0.003 0.003 0.003

0.006 0.006 0.006 0.006

>%>> >%>> >%>> 6%>>

6%>> 6%>> 6%>> 6%>>

6%<> 6%<> 6%<> 6%<>

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37.29 37.29 37.29 34.70

40.08 40.08 40.08 37.30

;>%>> ;>%>> ;>%>>

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Start &ruise Bac5 End &ruise Bac5 Start ,andin ,oiter End ,andin ,oiter

6b 6 6L 69a

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6%><9 6%><9 6%>6 6%>6

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6:%:6 6:%6 6:%6 6:%6

1.00 1.00 1.04 1.04

13.16 12.71

0.00 0.00 7.73 7.73

0.000 0.000 0.474 0.4740.00 0.00 0.81 0.81

1.27 1.27

0.81 0.81

0.81 0.81 0.81 0.81

0.10 0.10 0.10 0.10

8.44 8.43 8.43 8.43

27.21 27.76 28.25 28.25

34.01 34.70 35.31 35.31

36.56 37.30 37.84 37.84

34.01 34.70 35.31 35.31

36.56 37.30 37.84 37.84

0.021 0.021 0.021 0.021

0.032 0.032 0.032 0.032

0.003 0.003 0.003 0.003

0.056 0.056 0.056 0.056

0.84 0.87 0.90 0.90

14.57 14.57 14.57 14.57

1.797!05 1.833!05 1.869!05 1.869!05

0.003 0.003 0.003 0.003

0.006 0.006 0.006 0.006

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36.56 37.30 37.84 37.84

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6:%6 6:%6 6:%6 6:%6

>%>> >%L >%>> >%L<

>%:= >%:= >%; >%;>%<6 >%<> 6%>> 6%>>

>%>L >%>9 >%>9 >%>9

:L%> :L<%96 :L% :L%

%L %9 %> %>

>%>6 >%>6 >%>; >%>;

;=%;6L ;=%:> ;=%:> ;%:>

>%>>> 6%= >%>>> 6L%:9

50 47 27 25

Start ,andin ,and #a*i bac5 Enine shut do1n

69b :>a :>b :6

>%L> >%> >%> >%>

6%< 6%: 6%: 6%:

>%:> >%>> >%>> >%>>

>%9<9 >%9=<9 >%9=<9 >%9=<9

6%>LL= 6%>L99 6%>L99 6%>L99

>%L>L >%L6 >%L6 >%L6

6%>6 6%>L< 6%>L< 6%>L<

9%;L:E@>; 9%;9;E@>; 9%;9;E@>; 9%;9;E@>;

6:%6 6:%6 6:%6 6:%6

1.00 1.00

0.00 0.00

0.000 0.0000.00 0.00

0.81 1.35

0.10 0.10

8.43 14.02

27.76 26.92

34.70 26.92

37.18 28.77

34.70 26.92

37.18 28.77

0.021 0.000

0.032 0.000

0.003 0.000

0.056 0.000

0.87 0.00

14.57 0.00

1.837!05 0.000!00

0.003 0.000

0.006 0.000

>%6= >%6= >%6= >%>>

6%>> 6%>> 6%>> 6%>>

6%<> 6%<> 6%<> 6%<>

>%L> >% >%= >%=

9%L> 66%9 6<%= 6<%=

6L%<< 6L%<< 6L%<< 6L%<<

>%>> >%>> >%>> >%>>

6%LL 6%=< 6%: 6%:

>%L> >%> >%> >%>

6%>> :%>>

;:%>> ;:%>>

;<%:9 ;<%69

34.70 26.92

37.18 28.77

>%6= >%6= >%6=

>%6= >%6= >%6= >%>>

9%L> 66%9 6<%= 6<%=

<<%66 <=%:% :% :% >%>>

6:%6 6:%6 6:%6 6:%6

>%>> >%9 >%> >%>6

;%:> ;%:> ;9%:> ;9%:>

6L%:9 6L%;:L 6L%;:L 6L%;:L

Dnputs

32.1'4100

$el Standard Day S,S0 Barometric 2ressure in-H0 29.920000

S,S temp de-(0 288.10000

0.0023'B9

S,S $iscosity mu> lbm.ft sec0 0.0000120

29.200000

2'.100000

Field ele$ation (ft0 0.B00000

>i##ion Segment

Segment 0

0!B00 0!B00

6%:: 6%::

>%9=<9 >%9=<9

0.9959 0.9959

287.0 287.0

314.1 314.1

6%>L99 6%>L99

>%L6 >%L6

#AS.&AS 1.0B84 1.0'

1.0699451 1.0699451

9.39'E<03 9.39'E<03

Standard ra$ity ft.sec2) or ra$ity constant ftlbm.lbf sec:0

S,S density 3ho> lbf-sec: .ft<

Field Barometric 2ressure [in-H!" - referenced toseale$el

Ambient temp abo$e std% day ∆

ta 0at field ele$ation

[de&!"

light 9eady atFeld elevation

Engine Startand Chec;

>S, mi##ion altitude (h/) G?&tH3

Field non-std dayδ

at seale$el pa .p

>0 7 2

baro .:9%9:

Standard day pressure altitude correction ∆hp0 for

non-standard 2baro

relati$e to sea le$el

>S, #tandard day pre##ure altitude (hp #td

(?&t) altimeter reading $hen altimeter#et &or 2 !2 in-.g

δ calculated from hp std0

Standard day ambient temperature ratio ta .t

>0 7 θ

Std day temp ta std

4on-std day temperature ta

in de(0

4on-std temperature ratio θ

4on-std day density ratio σ

city ratioµ µ

nd0 - from Sutherland?s appro*imation

3n.l (&AS

(ey" ,abel

Input $alue

&alculation transferred to &ommonData

<al#ulati%n n%t trans*erred t% <%--%nata

3 4 B ' 8

ai out #a5eoff run 3otate ,iftoff Start &limb End Clim"

1 2a 2" :a :" :!a

0!B00 0!B00 0!B00 0!B00 0!B00 1!000

6%:: 6%:: 6%:: 6%:: 6%:: 6%:

>%9=<9 >%9=<9 >%9=<9 >%9=<9 >%9=<9 >%9<6>

0.9959 0.9959 0.9959 0.9959 0.9959 0.9931

287.0 287.0 287.0 287.0 287.0 286.2

314.1 314.1 314.1 314.1 314.1 313.3

6%>L99 6%>L99 6%>L99 6%>L99 6%>L99 6%>L:

>%L6 >%L6 >%L6 >%L6 >%L6 >%L=

1.0' 1.0' 1.0' 1.0' 1.0' 1.0'

1.0699451 1.0699451 1.0699451 1.0699451 1.0699451 1.0678476

9.39'E<03 ??? 9.39'E<03 9.39'E<03 9.39'E<03 9.39E<03

9 10 11 12 13

tart AccelEnd Accel

:!" 4a 4" Da 10"

1!000 1!000 1!000 1!000 1!000

6%: 6%: 6%: 6%: 6%:

>%9<6> >%9<6> >%9<6> >%9<6> >%9<6>

0.9931 0.9931 0.9931 0.9931 0.9931

286.2 286.2 286.2 286.2 286.2

313.3 313.3 313.3 313.3 313.3

6%>L: 6%>L: 6%>L: 6%>L: 6%>L:

>%L= >%L= >%L= >%L= >%L=

1.0' 1.0' 1.0' 1.0' 1.0'

1.0678476 1.0678476 1.0678 1.0678 1.0678

9.39E<03 ??? 9.39E<03 9.39E<03 9.39E<03

Start Crui#e8ut

End Crui#e8ut

Start Search -,evel light

14 1 1B 1' 18

11 12a 12!a 12!" 1:a

1!000 1!000 1!000 1!000 1!000

6%: 6%: 6%: 6%: 6%:

>%9<6> >%9<6> >%9<6> >%9<6> >%9<6>

0.9931 0.9931 0.9931 0.9931 0.9931

286.2 286.2 286.2 286.2 286.2

313.3 313.3 313.3 313.3 313.3

6%>L: 6%>L: 6%>L: 6%>L: 6%>L:

>%L= >%L= >%L= >%L= >%L=

1.0' 1.0' 1.0' 1.0' 1.0'

1.0678 1.0678 1.0678 1.0678 1.0678

9.39E<03 9.39E<03 9.39E<03 9.39E<03 9.39E<03

End Search -,evel light

Start Search -urn#

End Search -urn#

Start Surveil -urn#

End Surveil -urn#

19 20 21 22 23

1:" 1B" 1D 1I 1a

1!000 1!000 1!000 0!I00 0!I00

6%: 6%: 6%: 6%<: 6%<:

>%9<6> >%9<6> >%9<6> >%9<9 >%9<9

0.9931 0.9931 0.9931 0.9945 0.9945

286.2 286.2 286.2 286.6 286.6

313.3 313.3 313.3 313.7 313.7

6%>L: 6%>L: 6%>L: 6%>LL= 6%>LL=

>%L= >%L= >%L= >%L>L >%L>L

1.0' 1.0' 1.0' 1.0' 1.0'

1.0678 1.0678 1.0678 1.0689 1.0689

9.39E<03 9.39E<03 9.39E<03 9.3'8E<03 9.3'8E<03

*ayloaddrop

Start Crui#e+ac;

End Crui#e+ac;

Start ,anding,oiter

End ,anding,oiter

24 2 2B 2'

Start ,anding ,and ai "ac;

1" 20a 20" 21

0!I00 0!B00 0!B00 0!B00

6%<: 6%:: 6%:: 6%::

>%9<9 >%9=<9 >%9=<9 >%9=<9

0.9945 0.9959 0.9959 0.9959

286.6 287.0 287.0 287.0

313.7 314.1 314.1 314.1

6%>LL= 6%>L99 6%>L99 6%>L99

>%L>L >%L6 >%L6 >%L6

1.0' 1.0' 1.0' 1.0'

1.0689 1.0699 1.0699 1.0699

9.3'8E<03 9.39'E<03 9.39'E<03 9.39'E<03

Engine #hutdo$n

2recoded cells representin ad$anced options not re/uired for ASE ;6 desin

Iteration K

$erall inputs

+in loadin

2o1er-to-1eiht r

Assessments options

Si'in options

6% Fi*ed eometry VS2 baseline Sref 7 const8 S1et.Sref 7 const8 +af.Sref 7 as input0

:% Fi*ed eometry VS2 baseline Sref 7 const8 S1et.Sref 7 const8 +af.Sref 7 as calculated0

<% Variable eometry VS2 baseline - ,i5e option ; e*cept fuselae.pod and nacelle scaled to meet $olume re/u

Bottoms up mass mass estimate inputs

Fi*ed baseline desin options 6-;0 or initial estimate options >8 <0 ta5eo

3etained internal payload 1eiht -

3etained e*ternal payload 1eiht -

E*pended internal payload 1eiht - un

E*pended e*ternal payload 1eiht - uni

Fuel or battery 1eiht fraction - ins

Enine or )otor 2o1er-to-+eiht 3atio BHp>.+

Enine or )otor Installation +eiht factor +e

2arametric airframe 1eiht multipli

Iterate bottoms up 1eiht B+0

3etained internal payload 1eiht as input -

3etained e*ternal payload 1eiht as input-

E*pended internal payload 1eiht as input - un

E*pended e*ternal payload 1eiht as input- un

ninstalled enine or mot

;% Variable 1in and tail eometry8 VS2 baseline fuselae.nacelle.pod eometry fi*ed8 +>.Sref si'ed 1in8 tail si'ed by #V&8 +af.Sref as calculated

=% Scaled parametric eometry8 initial S1et.Sref definition8 Sht.Sref and S$t.Sref 7 const8 +af .S

ref 7 airframe 1e

* >%:9O+> .S

ref 0>%<

Systems@a$ionics 1eiht fraction - inst

4ose ear 1eiht fraction - ins)ain ear 1eiht fraction - inst

Empty 1eiht ro1th marin fra

)isc% +eiht Fraction - installed +m

Input airframe unit 1ei

&alculated A parametric airframe unit 1ei

Iterated bottoms up ross 1eiht from pre$ious iteratio

For si'in options 6 G :8 Sref 7 baseline 1in reference area as input belo18 if option J : calculate S ref iter from

Fuel or battery 1

ninstalled enine or motor po

)isc% 1eiht -

Bottoms-up calculated +Bottoms up 1in loadin +>.Sref - psf0 - calculate con$e

Bottoms up useful load , - lbm0 - calculate con$e

Airframe 1eiht fraction +af.+>0 - calculate con$e

Empty 1eiht fraction +e.+>0 - calculate con$e

Density Inputs

3etained internal payload density8 inst

3etained e*ternal payload density8 inst

E*pended internal payload density8 inst

E*pended e*ternal payload density8 instFuel or battery0 density8 inst

Enine or motor0 density8 inst

Systems@A$ionics +eiht density8 insta

4ose ear density8 inst

)ain ear density8 inst

+eiht ro1th marin density8 inst

)isc% +eiht density8 inst

Volume marin

Volume marin fraction re/?d Vol ma

&alculate $olume re/uired

3etained internal payload $olu

3etained e*ternal payload $olu

E*pended internal payload $olu

E*pended e*ternal payload $olu

Fuel or battery located in.or body $olu

Installed propulsion $olu

Systems

Installed enine or motor 1eih

Systems@a$ionics and landin ear desin 1eiht for ption J ; use +>iter8

else use input +> [lbm! - E*am

Systems@a$ionics 1eiht - installed lbm

4ose ear 1eiht - installed lbm

)ain ear 1eiht - installed lbm#otal alihtin ear 1

Airframe 1eiht +af [lbm!" for si'in option J68 calculate +af from pre$ious +

iter and S

ref iter8for first iter u

Airframe 1eiht +af [lbm!" for si'in option J<8 calculate +af from input alorithm8 else +af from abo$e - Anot

Empty 1eiht ro1th ma

Empty +

Empty 1ei

Volume marin cuft0 7 sum O

#otal $olume

#otal $olume re/?d less p

2arametric eometry definition

@ing E

Airfoil ma*imum thic5ness location

+inlet planform area fraction - both sides S1

Hori'ontal tail planfrom area fraction Sht.

Vertical tail planfrom area fraction S$t.S

+inlet and empennae S1et.

Baseline eometry definition

Baseline 1in reference area Sref0

Baseline 1etted area ratio S1e

S/rt&oe

2arametric eomerty calculations

+in reference area - copy Sref as ca

+in 1etted area - S1et 1e*p s/ft0 - f

+inlet planform area - both sides S1nlt s/ft0 - from

+inlet 1etted area - both sides S1et 1nlt s/ft0 - f

Hori'ontal tail planform area - Sht s/ft0 - calc

Hori'ontal tail 1etted area - S1et ht s/ft0 - f

E*posed 1in planform area fraction - S1e*p

Baseline fuselae@nacelle@pod 1etted area as dra1

Baseline 1in span ft0 - f

4ominal 1in body intersection diameter Dbi0 to span ratio /uadratic &oefB 7:.#3-60 - see handou

&oef& 7 #3@60.#3

Uuadratic s

Startin baseline body diameter at 1in inter

+in e*posed area fraction calculated from pre$ious scaled Dbi and span nd08 see hando

+in e*posed planform a

Hori'ontal tail area ratio - Sht .S

ref for si'in option ;8 use input Sht.Sref8 else use pre$ious iterated #V&

Hori'ontal tail area ratio - Sht .S

ref for si'in option 7 =8 use input Sht.Sref8 else u

Vertical tail planform area - S$

Vertical tail 1etted area - S1et $

+3oot chord - &r - calculate usin h

#ip &hord - &t - calcula

&mac lth - calcula

Baseline #ail eometry and Volume &oefficients

+inlet a%c% location

Hori'ontal #ail Volume &oefficient 7 ,ht.&

Vertical #ail Volume &oefficient 7 b.&

Hori'ontal tail momen

Vertical tail momen

Hori'ontal tail moment arm re/?d ,ht ft0 - from H#V& def?n and

Vertical tail moment arm re/?d ,$t ft0 - similar to ,ht e*cept 1

sin same e/uations also calculate

&alculated H#V& usin input tail moment arm and calculated 1in &mac an

Baseline unit 1eihts

Fuselae@nacelle@pod 1eiht per unit S1e

Vertical tail area ratio - S$t .S

ref for si'in option ;8 use input S$t.Sref8 else use pre$ious iterated #V&

Vertical tail area ratio - S$t .S

ref for si'in option 7 =8 use input S$t.Sref8 else u

+etted area ratio - S1et.Sref" for si'in option ; 8 use input S1et

.Sref8

else use pre$ious iterated bo

Scaled fuselae@nacelle@pod 1etted area S1et fnp iter

in s/ft0% For si'in option < 8 use input $alue8 els

Bottoms up total 1etted S1et iter

- sum of iterated $alues fro

Bottoms up 1etted area ratio

+in ma* chord thic5ness s1eep de0 + #al#ulate #%nv

+in body intersection diameter Dbi - ft0 + #al#ulate #%nv

+etted A3 b: .S1et0 + #al#ulate #%nv

+ith 1inlets V#V& 7 ,$t .b0S

ref 0 @ &

mac .b0S

1nlt .S

Sht .S

iter re/?d from H#V& def?n but multiply input ,ht by fuse@pod len

S$t .S

iter re/?d adusted for 1inlet contribution - other1is

&alculated V#V& usin input tail moment arm and calculated 1in span and tail area ratio% +inlet effect not

+in 1eiht per unit e*posed planform a

Empennae 1eiht per unit planform area

+fuse lbm0 - S1et f usin pre$ious scaled eometry from this

+nac+pod

Baseline B,0 eometry

Baseline eometry scalin

+in $olume scale factor calculated from ar

4acelle lenth scale factor calculated from $olum

4acelle area scale factor calculated from $olum

Fuselae@pod lenth scale factor calculated from $olum

Fuselae@pod area scale factor calculated from $olum

Scaled fuselae 1etted area - S1et-fuse s/ft0 7B, * fuse@pod arScaled nacelle 1etted area - S1et-nac s/ft0 7 B, * nacelle ar

Scaled pod 1etted area - S1et-pod s/ft0 7 B, * fuse@pod ar

Fuselae usable $

2od usable $

4acelle usable $

+in usable $

Iterate +af .S

[lbm! 7 1etted area S1e

+1 [lbm! 7 +in e*posed planfo

+af [lbm!

;use+age S*et

ace++e S*et

7od S*et

+in reference A3EA scale factor calculated usin iterated Sref from

+in ,E4#H scale factor calculated from ar

For option J ;8 nacelle $olume scale factor is defined by pre$ious iteration nacelle $olume re/?d. B, us$olume scale factor V

Similar to nacelle VSF8 for option J;8 fuse@pod $ol scale factor is defined by VSFfp iter

from pre$ious ite

Fuselae ross $olume

4acelle ross $olume

2od ross $olume

E*posed 1in ross $olume

Baseline 1etted area details

Volume a$ail $s% re/?d

Iterated ross fuselae $olume a$ailable cuft0 7 baseline fuse $ol * fuselae@pod0 $olume scal

Iterated ross nacelle $olume a$ailable cuft0 - similar e*cept based on nacelle $olu

Iterated ross pod $olume a$ailable cuft0 - also based on fuselae@pod0 $olu

Iterated ross 1in $olume a$ailable cuft0 7 baseline 1in $ol * 1in $olu

ross $olume a$ailable cuft0

&alculated ross density 7

E/ui$alent cylinder ,.D

sable fuselae $olume a$ailable cuft0 7 iterated ross fuse $olume a$ail * usable fu

sable pod $olume a$ailable

sable nacelle $olume a$ailable

sable 1in $olume a$ailable

sable $olume a$ailable cuft0

&alculated a$ailable density 7 B+.

2ropulsion nacelle0 $olume re/?d copy from installed propulsion $olume re/?d calculate

#otal $olume re/?d less propulsion copy from abo$e $ol re/?d calculations0 7 1in@fuselae@pod $olu

Fuselae@pod $olume re/?d cuft0 7 total $olume re/?d less propulsion minus 1in

+in $olume a$ail 7 1in@fuselae@pod $olume re/?d - fuselae@po

#otal usable $olume a$ailable.total $olume re/uired las

End of ;

)assVol3e/?d Cenhanced featuresC

2ropulsion nacelle0 $olume re/?d . usable nacelle $ol a$ail 7 nacelle $olume scale f

Fuselae @ pod $olume re/?d0.B, usable fuselae@pod $olume a$ailable0 7 $olume scale f

Airframe eometry Definition selected0

Body referenced nacelle 6 fraction of nacelle S1et S1et-

Body referenced nacelle : fraction of nacelle S1et S1et-

+in mounted nacelle ,6@36 fraction of nacelle S1et S1et-nac,6

+in mounted nacelle ,:@3: fraction of nacelle S1et S1et-nac,:

S1et fraction of pod referenced to body S1et-n1S1et fraction of pod referenced to 1in S1et-1

Body referenced )ass Fraction Distributions

Fraction of retained internal payload located in.on

Fraction of retained e*ternal payload located in.on

Fraction of e*pended internal payload located in.on

Fraction of e*pended e*ternal payload located in.on

Fraction of fuel or battery located in.or

Fraction of installed propulsion located in body referenced nace

Fraction of installed propulsion located in body referenced naceFraction of systems@a$ionics referenced to

Fraction of nose ear located in.on

Fraction of main ear located in.on

Fraction of empty 1eiht marin located in.on

Fraction of misc% 1eiht located in.on

+in 3eferenced )ass Fraction Distributions

Fraction of retained internal payload located in.on

Fraction of retained e*ternal payload located in.on

Fraction of e*pended internal payload located in.on

Fraction of e*pended e*ternal payload located in.on

Fraction of fuel or battery located in

Fraction of installed propulsion 1in mounted in ,6@36 nac

Fraction of installed propulsion 1in mounted in ,:@3: nac

Fraction of systems@a$ionics located in

Fraction of nose ear located in.on

Fraction of main ear located in.on

Fraction of empty 1eiht marin located in.on

Fraction of misc% 1eiht located in.on

+in and tail location Inputs

+> desin static marin fra

Airframe eometry - 2arametric Definition

+inlet a%c%

3etained internal payload located

4eutral 2oint ,ocation fr

Empty 1eiht marin located in

)isc% 1eiht located in

Body referenced located A<<>n

Body referenced n

Body refere

+in referenced mass

3etained internal payload located i

3etained e*ternal payload located in

E*pended internal payload located in

E*pended e*ternal payload located i

Fuel or battery locate

Installed propulsion 1in mounted in ,6@36

Installed propulsion 1in mounted in ,:@3:Systems@a$ionics locate

4ose ear located i

)ain ear located i

+in mounted nace

+in mou

)oments referenced to body

3etained internal payload mass located in.o

3etained e*ternal payload mass located in.o

E*pended internal payload located in.o

E*pended e*ternal payload located in.o

Fuel or battery located in.o

Installed propulsion located in body referenced nac

Systems@a$ionics located in.

4ose ear located in.o

)ain ear located in.o

Empty 1eiht marin located in.o

)isc% 1eiht located in.o

body referenced located na

body referenced loca

Hori'o

)oments referenced to 1in3etained internal payload located in.on 1in.&

3etained e*ternal payload located in.on 1in.&

E*pended internal payload located in.on 1in.&

E*pended e*ternal payload located in.on 1in.&

Fuel or battery located in 1in.&

Installed propulsion 1in mounted in ,6@36 nacelles.&

Installed propulsion 1in mounted in ,:@3: nacelles.&

Systems@a$ionics located in 1in.&

4ose ear located in.on 1in.&

)ain ear located in.on 1in.&Empty 1eiht marin located in.on 1in.&

)isc% 1eiht located in.on 1in.&

+in mounted nacelle ,6@36.&

+in mounted nacelle ,:@3:.&

+in mounted pod.&

+inlet.

Subtotal ):.

3e/?d FS

Body referenced densities rearraned to simplify computation

3etained internal payload density located i

3etained e*ternal payload density located i

E*pended internal payload density located i

E*pended e*ternal payload density located i

Fuel or battery density located

Installed propulsion density located in body referenced

Systems@a$ionics density located

4ose ear density located i

)ain ear density located i

Empty 1eiht marin density located i

)isc% 1eiht density located i

+in referenced densities rearraned to simplify computation

3etained internal payload density located

3etained e*ternal payload density located

E*pended internal payload density located i

E*pended e*ternal payload density located i

Fuel or battery located density located i

Installed ,6@361in mounted propulsio

Installed ,:@3:1in mounted propulsioSystems@a$ionics density located i

4ose ear density located i

)ain ear density located i

Empty 1eiht marin density located i

)isc% 1eiht ldensity located i

Volume re/uired for components located in.or body

3etained internal payload located in

3etained e*ternal payload located in

E*pended internal payload located inE*pended e*ternal payload located in

Fuel or battery located i

Installed propulsion located in body referenced n

Systems@a$ionics located in

4ose ear located in

)ain ear located in

Body referenced $olum

Volume re/uired for body referenced com

Volume re/uired for components in.or 1in for

3etained internal payload located in.on 1

3etained e*ternal payload located in.on 1

E*pended internal payload located in.on 1

E*pended e*ternal payload located in.on 1

Fuel or battery located in 1

Installed propulsion 1in mounted in ,6@36 nacel

Installed propulsion 1in mounted in ,:@3: nacel

Systems@a$ionics located in 1

4ose ear located in.on 1

)ain ear located in.on 1

Empty 1eiht marin located in.on 1

)isc% 1eiht located in.on 1

Body referenced $olum

Volume re/uired for components i

> 6 : ; < =

Direct Input

;%;6L>> 2AV input

>%66 #ransfer from &ommonData

#ransfer to &ommonData

&omputational &ell6 ran#&er to C5Aero

6%:699=9:

>%>>=>%>:<9

6:%<=> 6:%=> 6:%9= 6:%>= 6:%> 6:%>L

;%L;> ;%L;> ;%L;> ;%L;> ;%L;> ;%L;>

>%>>> >%>>> >%>>> >%>>> >%>>> >%>>>

>%6=> >%6=> >%6=> >%6=> >%6=> >%6=>

>%=>> >%=>> >%=>> >%=>> >%=>> >%=>>

>%>>> >%>>> >%>>> >%>>> >%>>> >%>>>

:%66 :%6= :%6 :%6 :%6 :%6

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