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NASA CR 152276 DOCUMENTATION OF THE ANALYSIS OF THE BENEFITS AND COSTS OF AERONAUTICAL RESEARCH AND TECHNOLOGY MODELS Volume I: Technical Report (N AS A-CR- 15227 8) DOCUllERTITIOll OF TRE N80-15865 AIALYSIS OF THE BBNBPITS AND COSTS OF AERONAUTICAL RESEARCH AND TFCB9OLOGY HODELS, VOtUlC I Final Report (561 International Unclas Corp., ffenlo Park, Calif.) 203 p 63/66 44233 J. C. Bobick R. L. Braun R. E. Denny July 1979 Distribution of this report is provided in the interest of infcrmation exchange. Responsibility for the contents resides with SRI International. Prepared under Contract No. NAS2-10026 SRI International 333 Ravenswood Avenue Menlo Park, California 94025 For Ames Research Center National Aeronautics and Space Administration Moffett Field, California 94035 https://ntrs.nasa.gov/search.jsp?R=19800007605 2019-02-16T23:39:56+00:00Z
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Page 1: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

NASA CR 152276

DOCUMENTATION OF THE ANALYSIS OF THE BENEFITS AND COSTS OF AERONAUTICAL RESEARCH AND TECHNOLOGY MODELS

Volume I: Technical Report

(N AS A-CR- 15227 8) DOCUllERTITIOll OF TRE N80-15865 AIALYSIS OF THE BBNBPITS AND COSTS OF AERONAUTICAL RESEARCH AND TFCB9OLOGY HODELS, V O t U l C I F i n a l Report (561 International Unclas Corp., ffenlo Park, Calif.) 203 p 63/66 44233

J. C. Bobick R. L. Braun R. E. Denny

July 1979

Distribution of this report is provided in the interest of infcrmation exchange. Responsibility for the contents resides with SRI International.

Prepared under Contract No. NAS2-10026

SRI International 333 Ravenswood Avenue

Menlo Park, California 94025

For

Ames Research Center National Aeronautics and Space Administration

Moffett Field, California 94035

https://ntrs.nasa.gov/search.jsp?R=19800007605 2019-02-16T23:39:56+00:00Z

Page 2: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Appendix A

COMMON 1\LOCK AND VARIABLE DEFINITION

Table A . l p resents canmon block d e f i n i t i o n and use information f o r

a l l cornnon blocks i n t he ABC-ART program. For each ccmmon block, t he

rout ines where va r i ab l e s i n t he block are i n i t i a l l y def ined, redefined,

and used a r e shown.

I n Tables A.2, A.3, and A.4 a lphabe t i ca l lists of a l l v a r i a b l e s i n

t he F lee t Accounting, Airframe Manufacturer, and Air Carrier Modules,

respec t ive ly , a r e presented. For each va r i ab l e , the mode type ( r e a l ,

i n t ege r , e tc . ) , t he m a n s by which values a r e assigned ( input , calcula-

t ion , e t c . ) , the dimension i f an a r ray , the parameters referenced by each

a r r a y subsc r ip t ( a i r c r a f t type, year, e t c . ) , t he common block membership,

t h e rou t ine where a va lue w a s i n i t i a l l y assigned, and the d e f i n i t i o n of

the v a r i a b l e a r e given. The codes used i n these t a b l e s a r e given i n foot-

no tes t o t he tab les .

Page 3: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

T a b l e A . 1

COHHON BLOCK D E F I N I T I O N AllD USAGE

BLOCK NAME

ACCASHF

ACCINCO

ACCOST

ACCL?S

CASHFLO

COHPCST

COSTOT

CSHFU)

CUML'T

DEIAY

DELIVER

D W ?

TN

INCOME

INDICES

L I F E T I H

MARKET

MAXP

KJDS

ORDER

PERIOD

PUrrDAT

POP

PRDSCHL

P R I C E 0

P R I N T

PRODIDS

P?~DUCT

R D T E ~

IS

USED

GSHFLU, INRR, INTROR

REVENUE, CASUFLW, INTROR

CASHFLU

BET, SHARE. CURVES

CASHFLW, INRR. INTROR

COHPCOS, CXSHFLW, INTROR

ACCOST, COHPCOS. COSTPR

ACCOST, COMPCOS

ACCOST, COSTPR

RDTE

PLANT, REVENlii. COWCOS ( i n a d v d

INPLANT, P W

O P L I F E . REPAY, DEPSUB, NETSUB. SUM, CFSUB, DCFSUB. OUTPUT, TAX

REVE?NE, CASHFLW, I N T M R

BET. AMORITZ, NODS, BUYS, PLOTSGL, INPLWT

PLANT. INPLANT

BET, BUYS

PLANT

BET, HODS

PLANT, REVENL'E, COMPCOS &ac tivd

RDTE

BET, CURVES, PLOTTER

BET, AMORITZ, BUYS, PLOTSCL, I N P U N T

PLANT, COWCOS (inactive)

ACPRICE, INPLANT, REVEMIE

INPLANT, INTROR

COMPCOS , INTROR

PUNT, COMPCOS

RDTE, C A S H ~ U , INTROW

i

DEFINED

CASHFLU

REVENUE

CASHFLU

SHARE

CASRFLU

COMPCOS

ACCOST, COHPCOS

ACCOST

ACCOST

RDTE

P W

INPLANT

REVENUE

BET

INPLANT

3 E T

PLANT

BET

PLANT

RDTE

BFP

BET

PLANT

AQRICE

INPLANT

COHPCOS

PL~NT

R M ~

ROUTINES UHERE CCMHON B U C K

REDEFINED

I N P W

Page 4: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

T a b l e A.1

C O M N BLOCK DEFINITION AND USAGE ( C o n c l u d e d )

- - --

A

- BLOCK NAMe

R U T n B L

RESULTS

SBhRES

STARTER

S T M T L T

STATLIST

TOTAL

TOTALS

TRDTEC

TLZCNP

I T S

-

BLOCK I S

USED

RDTE. INTROR

BET, MDDS, BUYS. P L o T s n

BET, SHhRE

BET, CURVES, PLOTITR, P L M S a

INPLANP. P m

BET, HODS, M R T I Z , PLOTSGL

PLANT, COP(PCOS, REVENUE

BET, SHARE

ACCOST, RDTE, COSTPR, COWCOS

ACCOST, COWCOS. COSTPR

P M , RDTE, COMPCOS (inactive)

DEFINED

RME

BET

SHARE

BET

IWLANT

BET

P U N T

BET

ACCOST

ACCOST

PLANT

ROUTINES WHERE COMMON a

REDEFINED

MODS

BET

PLANT

Page 5: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

g u

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0

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5% s e d

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a C P 0 '4 a," 4 P

a :1 $ 2 $ 2 a: Y

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'4 a P P ) h d rc u r 0)

39, 2P) 3 U S b W t . 1 6 C UP) a u . 4 6 a

a 6 1 0 6 a d 5 ; u 6 u r c r r o

r u c ~ a : q * a A P 4 ' -1. 3 2 3' QI o u o 0 ' 4 - 3

rc.4 0 u r r c r rcrc P ) Q I ~ Q I U 4 u rc C Y P ~ a % g $ 8 2 w r o u a

r i x c 6 ~ ) a 4 o P) r W 6

QI

o a * 2; 0 4 Y 6

r m m r x P) u Y o w 9;l z u c

> X= a 43 , : 3 2 : $ 2 ~ 2 0 4 m .4 u c o c a a u u a P) o u r r

c u c u X c A 2 c 8 8 c Y 2

6 P) '4 > C

0 g * 4 4 r c A' U " 0 31 O . 2 E W $ 2 2 4 2 ' 1 4 d . a r n r o v m o a m u z n r u h m

N

r & !i! i2 a

G w

E Z 2 U = 9 r c-' s s a rp c )+I c - c Lp

a a a

E t i E 3:s m m m

r U u n n r

In 4

e QD * 0

n

u u U 4 U U U U U U U

a u a a a a u a P a a a a

pD U U P z ~ a G k L E -

Page 6: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

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(C

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ual

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it n

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it n

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imum

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in-

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YR

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LI

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HL

IFE

TT

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m'

Page 7: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.2

(C

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dic

ato

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ear

for

mo

dif

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er o

f a

irc

ra

ft o

f each

typ

e placed

in

gh

t)

in each year.

ber

of

ex

1 .z

ing

air

cr

aft

ty

pes

in

a m

ar

Page 8: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

i

z 0

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&

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r. a, ; a * I a > a U Y C c * S r l 99 ) * g 4: rl 4 w 4 5 i . o a 2 2 4 , X

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9) 9)

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a o u w o u * a h 3 Jr.1," P I m & . 2

w * 0 u h rl P I : X z A X " $ h

h, u u a a JI; Y ) ; t i i 4 5 a 0

P n w . e 5 14 * 0 3 r( 0 !8- *. U S 9 ) . W 6 ii 2 6 M e a r U t u rl

a : 2 l 3 : flr*i I a . R a # W U r n ,a 2 4 C 0 P E 6 & r l r l a u a a 2 3 % w S S,C P w o r l a r l r

6 d 9) 9) u a " Z E R 1 a c t u

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ww a % u w h 0 4 wrl o w rl 4 8 ' B R a t 5 * E g 1 s a 2 g 94% g s . 9 ) o 2,C Gu$2;.tt

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N cl n " L C

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Page 9: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.2

(C

on

tin

ued

)

t V

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IAB

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NAUE

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IST

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imum

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e

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ie (

Y-a

xis

) o

f p

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.

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tal

WH

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ila

ble

in

a m

ark

et

in a

giv

en

ye

ar

be

fore

air

cra

ft b

uy

s in

th

e y

ea

r.

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tal

num

ber

of

air

lra

ft

bo

ug

ht

in

al

l m

ark

eta

fnr

ea

ch

yea

r.

To

tal

fue

l co

nsum

ed

in

al

l m

ark

ets

in

eac

h y

ear.

-

DE

FIN

ING

R

OU

TIN

E

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BET

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RE

Page 10: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.2

(C

on

clu

ded

j

FOO

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Page 11: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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Page 12: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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Page 13: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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Page 14: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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C

I C

DSD

,I

VA

RIA

BLE

NA

ME

CFEN

AC

CFEN

G

CF

NS

Y

CFH

ND

L

CFH

YCD

CFI

NST

C FLG

CFN

AC

CFP

AC

C

CPP

NC

D

CFP

OU

CFT

REV

CFU

SYS

CR

JIN

G

CHAN

DL

CHY

CAD

CIN

ST

CIN

STE

CIN

ST

I

CLG

CNA

CEL

CO

)(E

NT

CO

HPC

ST

CO

NFI

G

TY

PE'

R R

R

R

R

R R

R

S

R R R

R

R

R R

R R

R

R

R

R

R R

IND

EXED

PA

RAME

TER^

DI

CU

D MO

COM

MON

BL

OCK

CO

UPC

ST

DE

FIN

ING

R

OV

PIN

E

AC

CO

ST

AC

CO

ST

ACC

OST

ACC

OST

ACC

OST

ACC

OST

AC

CO

ST

ACC

OST

AC

CO

ST

ACC

OST

AC

CO

ST

AC

CO

ST

ACC

OST

AC

CO

ST

ACC

OST

ACC

OST

AC

CO

ST

ACC

OST

ACC

OST

AC

CO

ST

ACC

OST

AC

PRIC

E

CObI

PCO

S

ACC

OST

Page 15: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.

3 (C

an

t in

ned

)

TYPE' R R R B

P R R

U E U R B R R U R R R I

B I I

VA

LUE

HO

DE

~

C

C

C

C C

C C C

C

C C

C

C

C

DSD, I

C

C

C

C

C

C

A

i

VA

RIA

BLE

?(

AXE

CO

ST

CPA

CCO

CPC

T

CPC

T I

CP

PC

CPWCAD

CPO

cw

C pr

o0

CPO

l

CPr

UEI

L

CPU

CA

CS

fPU

C

CTJ

CIJ

I

CT

PE

VS

CY

CY

IW

WP

MJE

L

MIM

PL

DEL

AY

AB

AA

Y

DEM

ENSl

ON

37

~

3 1 5

INDE

XED

PA

RA

HE

TE

R~

W3 Y Q

l

C0

IW)H

BLOC

K

C?HO

Ut

CO

SW

(5 f

ac

tors

).

i

DE

PI)I

I!K

; PM

ITI!I

E

CA

SHFL

U

AC

CO

ST

AC

CO

ST

AC

CO

ST

ACC

OST

AC

CO

ST

AC

CO

ST

AC

CO

ST

ACCO

ST

ACC

OST

AC

CO

ST

A ,C

OST

AC

CO

ST

ACC

OST

ACCOST

IMBP

ACCOST

RmE

DESCRIPTION

Sum

o

f B

DTl

rE

ad

pro

du

cti

on

co

sts

each

mon

th.

Pa

sse

ng

er

ac

cd

at

io

na

and

furn

ish

ing

co

st.

Cu

mu

lati

ve

tota

l p

rop

rlsi

on

co

sts

fo

r (I

un

its

,

Cu

ou

lati

vr

tota

l p

rop

uls

ioa

co

sts

fo

r Q

-1 u

nit

s.

Pli

gh

t te

st

ve

hic

le p

rop

uls

ion

sy

stm

co

st.

Pn

eum

atic

oy

ste

r c

ost

.

Pro

du

cti

on

a

irc

raft

pro

pu

lsio

n s

yst

em

c

ost

.

Pro

pu

lsio

n c

os

t fo

r ea

ch u

nit

bas

ed

on l

ea

rnin

g

cu m

e.

Pro

prl

eio

r~ le

arn

ing

cu

Ne

fa

cto

r fo

r N

th

un

it.

Pro

pu

leio

n l

ea

rnin

g c

urv

e f

ac

tor

for

Hls

t u

nit

.

Au

xil

iary

po

ver

sy

stem

co

st.

Cu

ru

lati

vr

av

era

ge

un

it p

rop

uls

ion

co

at

for

C(

un

ite

.

Ase

rrb

led

a

irp

lan

e c

os

t.

Air

pla

ne

en

gin

e u

nit

co

bt .

Inp

ut

va

lue

fo

r a

irp

lan

e e

ng

ine

un

it c

os

t.

Yl~

ms

t rw

ers

er

co

st.

To

tal

air

cra

ft

ma

nu

fac

turi

ag

c

ost

.

Win

g c

os

t.

Dis

cou

nte

d

ca

sh f

luu

fo

r each

ye

ar.

Air

fra

me

de

sig

n a

nd

de

ve

lop

ea

t e

ng

ine

eri

ng

c

ost

.

La

st w

nth

be

fore

de

liv

ery

mon

th.

Del

ay

be

fore

RD

YE

com

po

nen

t w

et

sta

rts

Page 16: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.3

(C

on

tin

ued

)

VA

RIA

BLE

NA

UE

DEL

IVER

DEL

TAP

DEL

TAR

DEL

SCH

L

DEUA

ND

DIS

CR

EP

DS EA

IRFP

EAIB

PR

mzv

c EE

NCP

R

EN

EN

END

l

END

l

END

2

ENSP

AO

ENSP

AR

EPR

ICE

ESE

PRI

--

VA

LUE

me

2

C

C

A C

C

C

C

C

C

C

C

I

DSD

.1

C

C

DSD , I

DSD

, I

C

C

AR

RA

Y

DIM

ENSI

ON

D

EFI

NIN

G

RO

UTI

NE

IND

EXED

PA

RAM

ETER

DEH

AN

D

CO

STO

T

COHH

ON

BU

)CK

INPL

AN

T

INR

R

PLA

NT

INPU

WT

PU

NT

I A

CC

OST

AC

PRIC

E

AC

PRIC

E

AC

PRIC

E

AL

nRIC

S

ACP

R IC

E

ACC

OST

PLA

NT

COH

PCO

S

PLA

NT

ACC

OST

ACC

OST

ACL

PRIC

E

AC

PRIC

E

DE

SCR

IPT

ION

Ho

nth

in

wh

ich

e

ac

h u

nit

vi

ll

be

de

liv

ere

d

(nam

e as

PRO

DU

CT)

.

Incr

emen

t fo

r a

irc

raft

pri

ce

.

Ch

ang

e i

n r

ate

fo

r p

rese

nt

va

lue

ca

lcu

lati

on

s.

Cu

mu

lati

ve

mb

er

of

un

its

de

liv

ere

d e

ac

h

mo

nth

(s

ame

as

PU

DSC

HL)

.

No.

o

f o

ne

new

air

cra

ft t

yp

e d

eman

ded

ea

ch

year,

Dis

cre

pa

nc

y b

etv

ee

n p

rod

uc

tio

n

po

ari

ble

and

de

mn

de

d .

Res

earc

h,

dev

elo

pm

ent,

te

st and

ev

alu

ati

on

su

pp

ort

.

Est

ima

ted

a

irfr

am

e p

ric

e.

Est

ima

ted

air

pla

ne

pri

ce

.

Est

ima

ted

a

irp

lan

e d

evel

op

men

t c

oa

t.

Est

ima

ted

e

ng

ine

s to

tal

pri

ce

.

Num

ber

of

mai

n e

ng

ine

s

Num

ber

of

mai

n

en

gin

es.

La

et

mo

nth

in

pro

du

cti

on

sc

he

du

le f

or

pe

rio

d 1

.

Not

u

sed

.

La

st m

onth

in

pro

du

cti

on

sc

he

du

le f

or

pe

rio

d

2.

Hai

n e

ng

ine

sp

are

s fa

cto

r,

pro

du

cti

on

ph

ase.

Mai

n e

ng

ine

sp

are

s fa

cto

r,

RDTL

E p

has

e.

Est

ima

ted

air

pla

ne

ma

rke

t p

lac

e p

ric

e.

Est

ima

ted

a

irp

lan

e p

ric

e b

y s

ea

t c

os

t,

mil

lio

ns

Page 17: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A. 3

(Co

nti

nu

ed)

-

VA

RIA

BLE

NA

HE

FAC

PAC I

WE

FEE

PIR

STPR

IT1

FPR

OD

1

FPR

OD

2

Fro

Fro1

IT

S

W

PVCT

WC

TI

WSP

AB

mc

mu

CFS

GTS

PAR

GTV

HP I IA

UCCUH

VA

LUE

HODE~

C

DSD

,I

DSD

. I

I C

C C

C

C

DSD , I

C C

C

C

DSD

, I

C

C C

DSD

, I

C I LI

C

C

ARR

AY

D

IHE

tiSIO

N

IND

EXED

PA

BA

HET

ER

CO

STO

T

CUH

OU

T

CO

STO

T

CO

STO

T

CO

STO

T

CUW

OUT

ClR

lOU

T

CUH

DU

T

CUH

OU

T

CO

STO

T

I i i

DE

FIN

ING

R

OU

TIN

E

ACC

OST

AC

CO

ST

ACC

OST

ACP

R I CE

PLA

NT

PIA

NT

PLA

NT

PU

NT

ACC

OST

ACC

OST

ACC

OST

AC

CO

ST

AC

CO

ST

ACC

OST

ACC

OST

ACC

OST

ACC

OST

ACC

OST

AC

CO

ST

ACC

OST

AC

PltI

CE

INP

MT

AC

PRIC

E

PLA

NT

DE

SCR

IPT

ION

Pro

du

cti

on

fa

cil

itie

s c

oa

t.

Inp

ut

va

lue

of

pro

du

cti

on

f

ac

ilit

ies

co

st.

hn

ufa

ctu

rer

fee

fa

cto

r.

Not

u

sed

.

No.

o

f y

ea

rs i

n f

ira

t p

eri

od

.

Po

inte

r to

fir

st

ye

ar

of

pe

rio

d

2.

Ac

tua

l tr

on

thly

p

rod

uc

tio

n r

ate

fo

r p

eri

od

1.

Ac

tua

l m

on

thly

pro

du

cti

on

ra

te f

or

pe

rio

d

2.

Pli

gh

t te

st

op

era

tio

n c

ost

.

Inp

ut

va

lve

fo

r fl

igh

t te

st

op

era

tio

n c

ost

.

Fli

gh

t te

at

air

cra

ft s

pa

res

co

st.

Fli

gh

t te

t~t v

eh

icle

s w

et.

Cu

mu

lati

ve

tota

l a

irp

lan

e c

os

ts f

or

Q

un

its

.

Cu

mla

tiv

e

tota

l a

irp

tcrn

e c

os

ts f

or Q

-1 u

nit

s.

Pli

gh

t te

et

ve

hic

le s

pa

res.

Un

it a

irp

lan

e c

os

t o

f Q

-th

u

nit

.

Cu

mu

lati

ve

av

era

ge

un

it a

irp

lan

e c

os

t fo

r Q

u

nit

s.

Gro

un

d

tes

t v

eh

icle

sp

are

s c

oa

t.

Gro

un

d

tee

t v

eh

icle

sp

are

s fa

cto

r.

Gro

und

tes

t v

eh

icle

s c

ost

.

En

gin

e d

esi

gn

sh

aft

ho

rsep

ow

er.

Loo

p in

de

x (

mu

ltip

le u

ses)

.

Ind

ica

tor

use

d

in e

stim

ati

ng

air

pla

ne

co

st.

Rou

nded

(u

p b

y .6

7) eru

of

un

its

dm

an

de

d.

Page 18: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Tab

le A

. 3

(Co

ntf

nu

cd)

IAIR

PL

I B

ICN

T

ICO

NFG

ICW

IDA

TA

IDIF

F

IEN

GS

I I

IL

IW

1

IHA

X2

IHIN

l

IHIN

2

-- VALU

E U

OD

E~

I LI

C

DSD

, I

C

I D

SD,I

1 C

I I 1

1

1 L

I

C

C

' C

C

C

ARR

AY

D

UE

NSI

OY

- ,.-

IND

EXED

I COH

HON

PARA

MET

EX

BLOC

K D

EFI

NIN

G

RO

UTI

NE

AC

PRIC

E

PU

NT

I NRR

ACC

OST

ACC

OST

ACC

OST

PLAN

T

AC

PRIC

E

AC

PRIC

E

INR

R

PLANT

PLANT

PU

NT

PLA

NT

DE

SCR

IPT

ION

Ind

ica

tor

for

air

pla

ne

ty

pe.

IA

IRPL

-1

for

co

nv

en

tio

na

l J

et

tra

ne

po

rte

. IA

JRPL

-2

for

smal

l je

t tr

an

spo

rts.

IA

IRPL

-3

for

wid

e bo

dy

jet

tra

nsp

ort

s.

IAIB

PL-4

fo

r tu

rbo

-pro

p

tra

nsp

ort

s.

IAIR

PL-5

fo

r g

en

era

l a

via

tio

n t

yp

es.

IAIR

PL-6

fo

r su

pe

rso

nic

tra

nsp

ort

s.

Loo

p in

dex

- st

ar

ts a

t 2

.

Co

un

ter

to f

ind

ev

ery

10

th c

yc

le.

Ind

ica

tor

for

air

cra

ft t

yp

e,

(6 =

eu

beo

nic

p

rod

uct

ion

, 7

= p

roto

typ

e,

8 - su

pe

rso

nic

p

rod

uct

ion

).

Ind

ica

tor

for

cum

ula

tiv

e q

ua

nti

ty.

Not

u

sed

.

Dif

fere

nc

e b

etw

een

last

mon

th o

f ea

ch d

eman

d y

ear

and

mon

th

las

t u

nit

ech

edu

led

fo

r pr

oduc

- ti

on

.

Ind

ica

tor

for

typ

e o

f en

gin

es.

IEN

GS-

1 fo

r tu

rbo

jet

and

turb

ofa

n.

IEN

CSu

2 fo

r tu

rbo

pro

p.

IEN

CS-

3 fo

r re

cijr

roca

tin

g.

IEN

CS-

4 fo

r a

irb

rea

thin

g.

Loo

p in

dex

.

La

st v

alu

e

of

loo

p i

nd

ex.

Tem

pora

ry

to f

ind

la

rge

et

dif

fere

nc

es

in p

eri

od

1

I ~e

m~

or

ar

~

to f

ind

la

rge

st

dif

fere

nc

es

in p

eri

od

2

iTem

pora

ry

to f

ind

la

rge

et

dif

fere

nc

es

in

pe

rlo

dl

Tem

po

rary

to

fin

d l

arg

es

t d

iffe

ren

ce

s in

pe

rio

d2

Page 19: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Table

4.3

(C

on

tin

ued

)

VA

RIA

BLE

YA

HE

ImT

H

IN

IN

m

IOP

S

IP

IPO

WER

IPR

OD

IQ

IR

IS

IT

ITH

ITH

PL

ITO

TAL

ITO

TA

Ll

ITO

TALZ

IV

1W.G

I Y EA

R

IYR

VA

LUE

UO

DE

~

C

C

C

DSD

, I

C

DSD

, I

DSD

, I

DSD

,I

LI

C

C

LI

LI

C

C

C

C

DSD

, I

C

C - A

my

D

IMEN

SIO

N

INDEXED

PARA

MET

ER

STA

RTU

P

PRL

Ur

1 CU

HO

UT

I CUH

OV

T I I I I i 1 TO

TAL ~ 1 I I I I I

DEF

ININ

G

RO

UTI

NE

INPI

AN

T

RDTE

REV

ENU

E

ACC

OST

INPW

NT

ACC

OST

ACC

OST

ACC

OST

I NTR

OR

INR

R

ACC

OST

CASH

PLW

PLA

NT

PLA

NT

PLA

NT

PLA

NT

ACC

OST

AC

CO

ST

PLA

NT

INP

UN

T

--

DE

SCR

IPT

ION

Mon

th

in w

hic

h d

eman

d b

eg

iaa

(y

ea

rs s

ince 1

974

x 1

2).

Sta

rtin

g m

on

th

for

each

BDTE

com

po

nen

t.

To

tal

rev

en

ue

(i

nco

me)

e

ac

h s

ep

ara

te m

on

th.

Ind

ica

tor

fo

r t

yp

e o

pe

rati

on

al

pro

gra

m,

1 =

con

mrr

rcL

a1 a

irli

ne

, 0 - o

the

r.

Pri

nt

fla

g f

or

mo

nth

ly c

os

t,

inco

me.

an

d c

aeh

- fl

ow

ta

ble

e

in I

NTB

OR

(O

lpri

nt,

1-

no

pri

nt)

.

Not

u

eed

.

Ind

ica

tor

for

pro

toty

pe

or

pro

du

cti

on

to

oli

ng

;

1 =

pro

du

cti

on

, 0 - p

roto

typ

e.

Ind

ica

tor

for

air

cra

ft q

ua

nti

ty m

atr

ix.

Po

inte

r to

mo

nth

wit

hin

lo

op

s,

Sta

rtin

g v

alu

e o

f lo

op

in

de

x.

In

itia

l fl

igh

t cr

ew t

rain

ing

co

st

for

NV

a

irp

lan

es.

Com

pone

nt

loo

p i

nd

ex.

Un

it

loo

p i

nd

ex

po

inte

r.

Num

ber

of

un

ite

in

pe

rio

d 1

.

Upw

ard

rou

nd

ed

(by

,6

71

nu

mbe

r o

f w

ho

le a

irc

raft

de

man

ded

in p

eri

od

1.

Upw

ard

rou

nd

ed

(by

-6

7)

nu

nb

er o

f w

ho

le a

irc

raft

de

man

ded

in

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Page 20: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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Page 21: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Tab

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Page 22: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

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Page 23: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

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Page 24: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

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Page 25: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

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Page 26: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

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RIA

BL

E

NMlE

WE

VEL

CA

D

W 8

UEN

ACC

UEN

CS

WN

GS

VFU

SYS

UN

IOT

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OSS

UHAN

DL

UHYCAD

UIN

ST

WLC

ncC

oN

ULC

STR

WLC I R

S

WLCWSL

VN

AC

EL

WPA

CCO

up

An

WPX

AD

WPO

WER

UPP

RO

V

VA

LUE

UO

DE

~

I

DSD

, I

DSD

, I

DSD

, I

DSD

.1

I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DS

D,I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

DSD

, I

Drn

.1

DSD

, I

C

AR

RA

Y

DIM

EN

SIO

N

IND

EX

ED

,,

PAB

AM

ETEP

C

OW

N

BLOC

K D

EFI

NIN

G

RO

LT

INE

AC

PRIC

E

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

PRIC

E

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CC

ST

AC

CO

ST

AC

CO

ST

, AC

CO

ST

/ ACC

OST

1 AC

CO

ST L A

irc

raft

em

pty

we

igh

t.

Ele

ctr

ic p

ow

er c

on

ve

rsio

n a

nd

dis

trib

uti

on

sy

ste

m w

eig

ht.

Em

pen

nag

e w

eig

ht.

En

gin

e a

ccess

ori

es

we

igh

t.

En

gin

es

tota

l w

eig

ht.

En

gin

es

tota

l w

eig

ht.

Fu

el

syst

em

we

igh

t.

To

tal

fu

el

ve

igh

t.

Air

cra

ft g

ross

tak

e-o

ff

ve

igh

t (0

WG

UTO).

Lo

ad a

nd

ha

nd

lin

g a

yst

em

we

igh

t.

Hy

dra

uli

c p

ow

er c

on

ve

rsio

n a

nd

d

istr

ibu

tio

n

ay

ste

m w

eig

ht.

Inst

rum

en

t sy

ste

m w

eig

ht.

Ali

gh

tin

g g

ea

r s

ys

ta

we

igh

t.

AL

igh

tin

g g

ear

co

ntr

ols

we

igh

t.

Ali

gh

tin

g g

ear

stru

ctu

re w

eig

ht.

Tir

e w

eig

ht.

hle

els

sn

d b

;ak

e w

eig

ht.

En

gin

c n

ac

r ::

--?ig

ht

.

Pa

sse

ng

e

. ..

tio

ne

(a

nd

e

qu

ipm

en

t) w

eig

ht.

Pa

ylo

ad

-.. ,GL.

Pn

eu

ma

tic

k-

-r

and d

istr

ibu

tio

n s

yst

em

we

igh

t.

Au

xil

iary

po

wer

sy

nte

m w

eig

ht.

1 C;.P~

%C

rela

ted

su

bsy

ste

m

de

ve

lo

~n

t

co

st

Page 27: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.3

(C

on

tin

ue

d)

CO

WN

BLOCK

CS

HP

U)

VA

RIA

BLE

NA

HE

WR

EV

S

WIN

G

SA

M

AR

MY

D

U~

SI

ON

L

-

~P

E'

R

R R

IND

EXED

P

~R

D

EFI

NIN

G

RO

UTI

NE

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

AC

CO

ST

INPL

AN

T

INPL

AN

T

AC

CO

ST

AC

CO

ST

CO

UPC

OS

CO

UPC

OS

AC

CO

ST

AC

CO

ST

AC

CO

ST

ACC

OST

1 i

VA

LUE

MOD

$

DSD

. I D

SD.1

DSD

.1

DE

SCR

IPT

ION

Th

rust

re

ve

rse

r w

eig

ht.

Win

g v

eig

ht.

Av

ion

ics

.dev

elo

pm

ent

fac

tor.

Fin

al

asse

mb

ly-c

hec

k

ou

t c

os

t fr

ac

tio

n.

His

ce

lla

ne

ou

s eq

uip

men

t d

evel

op

men

t fa

cto

r.

Loop

Ind

ex

.

Loop

ind

ex

.

Air

f ra

we

pro

du

ct i

on

le

arn

ing

cu

rve

co

st

fac

tor.

Av

ion

ics

pro

du

cti

on

le

arn

?n

g c

urv

e c

os

t fa

cto

r.

Air

f ra

ae

le

arn

ing

cu

rve

fa

- to

r.

Av

ion

ics

lea

rnin

g c

urv

e f

ac

tor.

Air

fra

me

le

arn

ing

cu

rve

ex

po

nen

t.

Av

ion

ics

lea

rnin

g c

urv

e e

xp

on

ent.

En

gin

e le

arn

ing

cu

rve

ex

po

ne

nt.

En

gin

e p

rod

~c

tlo

n le

arn

ing

cu

rve

co

st

fac

tor.

DSD

.1

DSD

.1

LI

LI C

C

C

C

C

C

C

C

XFA

SS

Y

I R

XN

eV

YEAR

YR

Z U

UF

UV

ZETA

ZE

TM

ZETA

P

ZP

R I I R R R R R

R R R

Page 28: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

FOO

TNO

TES

'Typ

e o

f v

ari

ab

le c

lase

if ic

ati

on

:

I =

In

teg

er

R =

Rea

l

4 V

alue

mode

cla

ee

if ic

ati

on

e:

C

- Valu

e c

alc

ula

ted

in

pro

gram

I

-Rea

d

from

in

pu

t f

ile

D

SD - Da

ta

stat

emen

t d

efi

nit

ion

A

- V

alue

ass

ign

ed i

n p

rogr

am

LI

= L

oop

ind

ez

'1nd

exed

p

aram

eter

fo

r ar

ray.

:

Y =

Num

ber

of

Yea

rs

DI

= D

ata

item

Q

i - Co

mpo

nent

nu

mbe

r I40

= N

umbe

r of

m

nth

e

NA

= N

umbe

r o

f a

irc

raft

PE - P

ric

e e

atl

ma

tes

LC =

Lea

rnin

g c

urv

e s

tep

Page 29: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...
Page 30: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...
Page 31: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...
Page 32: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...
Page 33: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.4

(C

on

tin

ue

d)

Page 34: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Tab

le A

.4 (C

on

tin

ued

)

ARR

AY

D

LXEN

SIO

N

12

/17

DE

FIX

ING

R

OU

TIN

E

i IM

RX

ED

I

PAIU

ME

TE

R~

I I ST

I i I I I

DI

W ./

IND

IR

IND

IR

SUM

CPS

UB

DIR

ECT

INDIRECT

DCF

SUB

SUM

' SU

H

I S

UH

TA

X

SU

H

SUH

,TA

X

SU

H,T

AX

SIR

4

Sun

I i

IND

IR

DIR

ECT

I lMIR

SIP

l

I D

IREC

T 1

1M)I

R

I 1

DE

SCR

IPT

ION

.

Cru

ise

tim

e,

ho

urs

. 1

Num

ber

of

coac

h s

ea

ts.

Cu

mla

tiv

e t

ota

l an

nu

al r

evea

ue,

b

oll

ara

.

Cu

mu

lati

ve

tota

l n

et

cash

flo

w,

do

lla

rs.

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st p

er

cru

ise

mil

e p

er s

eat, d

oll

ara

. I

I C

um

ula

tiv

e to

tal

dis

cou

nte

d n

et

ca

sh f

lw,

do

lla

rs.

I I 1 C

ua

rla

tiv

e

tota

l d

ep

rec

iati

on

(d

ou

ble

de

cll

p

/ in

&,

do

lla

rs.

I I C

um

ula

tiv

e to

tal

earn

ing

s b

efo

re

tax

ee a

nd

inte

ree

t,

Co

lla

rs.

I I

I C

uu

lati

ee

to

tal

earn

ing

. b

efo

re mu, d

oll

ar0

4

1 Cum

ula

tiv

e to

tal

init

ial

Inv

ee

Pe

nt,

d

oll

ars

.

Cu

mu

lati

ve

inco

me

tax

sum

, d

oll

ars

.

I Cu

mla

tlv

e t

ota

l n

et

earn

ing

s,

do

llar

*.

Cu

mla

tiv

e t

ota

l o

pe

rati

ng

co

at,

d

oll

are

.

Cu

~u

lati

ve

tota

l y

ea

rly

pri

nc

ipa

l pa

ymen

t*

I d

oll

ars

.

Av

erag

e nu

mbe

r of

st

evar

dea

oeo

in

co

ach

.

Co

st p

er

tak

aoff

p

er

sea

t,

do

lla

rs.

I C

um

ula

tiv

e to

tal

ye

arl

y i

nte

rest

pay

meu

t,

do

lla

rs.

Co

st p

er

tak

eo

ff,

do

lla

re.

Page 35: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.4

(Continued)

Page 36: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

d a a a PL a m a LX a a a a a a m I-I

Page 37: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.4

(C

on

tin

ued

)

DSF

IKIK

C

RO

UTl

NE

DEP

SUB

NET

SUB

OPL

IFE

IN

PUT

S

INPU

TS

ItlD

IR

INPU

TS

REP

AY

DIR

EC

T

DEP

SUB

DEP

SUB

DEP

SUB

OPL

I FE

INPU

TS

DEP

SUB

DIR

EC

T

IND

IR

REPA

Y

INPU

TS

INPU

I?S

DEP

SUB

REPA

Y

REP

AY

DIR

EC

T

DE

SCR

IPT

ION

Loo

p in

dic

ato

r fo

r y

ea

r v

alu

e.

Inco

me

tax

, d

oll

ars

.

In

it

~a

l inv

estm

ent,

d

oll

ars

.

Ind

ire

ct

op

era

tin

g c

oe

te p

er

pla

ne

per

yea

r.

do

lla

re.

Ind

ire

ct

op

era

tin

g c

os

ts p

er

pla

ne,

d

oll

ars

.

To

tal

num

ber

of

ye

ars

un

der

co

nsi

de

rati

on

(s

et

at

15

).

Loo

p in

dex

.

Co

un

ter,

lo

op

in

dex

.

Loo

p in

dex

.

Beg

inn

ing

ye

ar

of

seco

nd

ha

lf

of

eco

no

mic

li

fe.

Loo

p in

dic

ato

r f

or

num

ber

of

air

cra

ft.

Loo

p in

dic

ato

r fo

r y

ea

r v

alu

e.

Air

cra

ft n

umbe

r fo

r p

art

icu

lar

inp

ut

da

ta s

et.

Loo

p in

dex

.

Num

ber

of

air

cra

ft b

ein

g c

on

sid

ere

d.

Not

IJ

SC

~.

Eco

nom

ic

life

, y

ea

rs.

Eco

nom

ic

life

, y

ea

rs.

Loo

p en

d in

dic

ato

r fo

r nu

mbe

r o

f y

ea

rs.

Num

ber

in c

rew

.

I i

I'

I !

AYF

AY

Dif

iirl

iBIO

S

25

,10

0

25.1

00

25

,10

0

100

12

2

7

T L--

I---

i i

1LG

EX

ED

(

~f

iX

A?

l~

~f

l~

Y ,A

Y ,A

Y,A

A

L'-R!>

ZLE

C

OX.

:GN

S

UC

K

IN

IN

IN

IN

. i V

.G.C

p XX

?lZ

I n?

~~

, :.

;O2B-

I

I R

R

I I I I I I I I I 1

I I I I I I 1

I I

I NCT

AX

ImIN

V

IOC

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l

IYEA

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n

nM

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AN

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LI C

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C I

Page 38: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Ta

ble

A.4

(C

on

tin

ued

)

-,

DE

SCR

IPT

ION

Num

ber

of

en

gin

es.

Num

ber

of

ee

atn

.

Num

ber

of

sta

ge

le

ng

ths

(up

to 1

2 f

or

DIR

EC

T,

up

to

17

fo

r IN

DIR

).

Net

e

arn

ing

s,

do

lla

re.

Fla

g

to r

ere

ad

nam

e li

st N

STA

GE.

Op

era

tin

g c

ost

, d

oll

are

.

Am

ount

o

f a

irc

raft

pri

ce

fin

an

ce

d,

do

lla

rs.

Pri

ce

of

new

air

cra

ft,

do

lla

rs.

Ye

arl

y p

rin

cip

al

paym

ent.

d

oll

ars

.

Pre

sen

t v

alu

e d

isc

ou

nt

fac

tor

Inte

res

t r

ate

fo

r PV

c

alc

ula

tio

n (

BD

I).

Rat

e o

f d

ep

rec

iati

on

.

Rat

e o

f c

lim

b a

t c

ruis

e a

ltit

ud

e,

fee

t p

er cia-

Ute

.

Ra

te o

f c

lim

b

(se

a l

ev

el)

, fe

et

pe

r m

inu

te.

Re

sid

ua

l fr

ac

tio

n o

f a

irc

raft

pri

ce

fo

r sa

lvag

e.

Mai

nte

nan

ce l

ab

or

rate

, d

oll

ars

pe

r h

ou

r.

Inte

res

t r

ate

fo

r re

pay

men

t o

f p

urc

ha

se l

oan

.

Ex

pre

ss t

on

s en

pla

ned

. I

Fre

igh

t to

ns

enp

lan

ed.

To

ns

of

ma

il c

arr

ied

pe

r fl

igh

t.

VA

LUE

I I C

C

C

AsC

C

C

A

C I I A I A

C C I

VA

RIA

BLE

N

MiE

NREN

GN

NRS

EAT

NSL

NTE

ARN

NU

STA

G

OPC

OST

PBC

OST

PRIC

E

PRIN

PV

R RA

TE

RCH

RC

SL

RES

RL

IRA

TE

RTE

RTF

RR

I

ARRA

Y D

IMEN

SIO

N

25

,10

0

25

,10

0

25

,10

0

25,1

00

25

10

0

10

0

~P

E'

I I I R

I ,A

El

R

R

B

R

R R

It R

R

R R

R R

R

COHH

ON

BLO

CK

IN

IN

IN

IN

IN

IN

IN

IN

IND

EXED

PA

BA

HE

TE

R

Y,A

Y,A

YsA

YsA

Y

A

A

DE

FIN

ING

R

OU

TIN

E

DIR

EC

T

DIR

EC

T

IND

IR

DIRECT

IND

IR

NET

SUB

DIR

EC

T

INPU

TS

REPA

Y

OPL

IFE

IN

PUT

S

REPA

Y

DC

PSU

B

DC

PSU

B

DEP

SUB

DIR

ECT

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IR

DIR

EC

T

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T

INP

WS

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IR

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IR

IND

IR

Page 39: I: Technical - NASA · c g c * srl 99) * 2 4: 45i. rl 4w oa 2 4 , x 8, 8iwt n u 0 pi * &icp ... cohhdn block results statlist statlist shares shares shares shares shares totals ...

Tab

le A

.r

(Co

nti

nu

ed)

DE

SCR

IPT

ION

tons o

f p

rop

ert

y

(car

go

) c

arr

ied

per

fl

igh

t.

Va

lue

of

air

cra

ft a

t e

nd o

f ec

onom

ic

lXfe

l d

oll

ars

.

DE

FIN

ING

R

OU

TIN

E

-

IND

IR

DEP

SUB

'fw

CO

WO

N

BLOCK

IN

IND

EXED

PA

RMET

ER

Y ,A

VA

RIA

BL

E

NME

RTP

SALV

AG

IN

SUM

Y

earl

y t

ota

l an

nu

al r

even

ue,

d

oll

ars

.

IND11

1 Block s

pee

d,

mph

.

Y ST

Y

SARE

V

S B

SCC

TYPE

'

R R

TAX

TAX

SUM

SUW

SUN

TAX

TAX

SUH

DIR

ECT/

IN

SIR

SUH

SUM

SUH

SUM,TAX

SU

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Appendix B

DESCRIPTION OF PLOTTER SOFTWARE ROUTINES

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Appendix B

DESCRIPTION OF PLOTTER SOFTWkXE ROUTINES

The plo t ted output of the F lee t Accounting Module is generated on

the ZETA PLOTTER 230, using a CDC 7600 computer. The p l o t t e r software

used by the F lee t Accounting Module is described i n t h i s appendix. This

software includes subroutines PLOT, SYMBOL, PLOTS, RSTR, LINAXS, and

NUMBER. The descr ip t ions provided here were extracted from i n t e r n a l

* NASA Ames documentation . Lis t ings of the source code f o r the routines

a r e provided i n Appendix C.

SUBROUTINE PLOT(X,Y,IPEN)

PLOT performs the basic p lo t t ing function of moving the pen from its

current locat ion t o a speci f ied locat ion with the pen e i t h e r up o r down.

X,Y - The coordinates ( i n inches) of the point t o which the pen is t o be moved. The pos i t ive X d i rec t ion is defined a s p a r a l l e l t o the margin of the p lo t t jng paper and toward the clean r o l l (package) of paper (i.e., from l e f t t o r i g h t i n the normal fashion a s one stands alongside the p l o t t e r i n the indicated pos i t ion) .

* L. C. Evans, "Memorandum f o r Systems Studies Divison Staff on P l o t t e r Sof mare," NASA-Ames MS: 202-8, Mof f ett Field, Cal i fornia (April 1974).

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IPEN - The mtlgnitude of lPEN s p e c i l ; t h e o p e r a t i o n t o be performed:

IPEN = 0 No change i n pen p o s i t i o n ; p r e s e n t pen l o c a t i o n is redef in& 3s (XIS).

- 1 Pen is moved t o (S,Y! wi thou t r a i s i n g o r lower ing t h e pen.

- 2 Pen is moved t o (S,Y) w i t h pen down.

- 3 Pen is moved t o (S,Y) w i t h pen up.

= 4 No pen movement; t h e c u r r e n t l o c a t i o n of t h e pen is r e t u r n e d i n (X,Y).

= 5 I n i t i a l i z a t i o n c u l l ; used by PLOTS.

= 6 Pen is moved t o a new "page", t h e p l o t t e r b u f f e r is dumped, and t h e p e r t i n e n t pa ramete r s a r e re- i n i t i a l i z e d , readying t h e p l o t sof cwarc' e i t h e r f o r t e r m i n a t i o n of t h e program o r f o r 3 new p l o t .

- 7 Used t o change t h e p l o t t i n g f a c t o r ( i f S ' 0) o r t h e p l o t t e r g r a i n ( i f S < 0 and Y > 6); tlo opers- t i o n i f S < 0 and Y i 0. T h i s v a l u e of IPEN should not h e used u n l e s s t h e u s e r is i s m i l i a r enough w i t h t h e c~ldin,g of PLOT td unders tand what e f f e c t s changes i n t h e s e v a l u e s w i l l I~uve.

- 8 Pen is r a i s e d bu t n o t moved.

= 9 Pen is lowered b u t no t moved.

= 1 0 (not c u r r e n t l v used) .

= 1 1 , 1 , 1 , 1 4 Same as IPEN = 1,2 ,3 ,4 , excep t t h a t p l o t is o f f s e t , s c d l e d , snd r o t a t e d .

= 20 Same as OPEN - 13, except t h a t pen p o s i t i o n is saved.

- , 2 2 3 Same as IPEN = 11,12,13, excep t t h a t pen move- ment is c a l c u l a t e d r e l a t i v e t o t h e pen p o s i t i o n saved from t h e l a s t c a l l t o PLOT w i t h IPEN = 20.

I n t b - c a s e of lPEN = -1,-2,-3,-11,-12,-13,-21,--12,-23, t h e a c t i o n is t h e same a s t h a t d e s c r i b e d above, b u t a f t e r t h e new pen locn- t i o n has been reached, i t is r e d e f i n e d a s t h e o r i g i n .

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SUBROUTINE S ~ ~ L (XUHC,YLLUC ,HEIGHT, BCD, ORIENT,NCHAR)

SYMBOL causes a s t r i n g of alphanumeric information to be plot ted.

XUHC,YLLHC - For the purposes of v isual iza t ion, each character can be thought of a s being drawn ins ide a rec tangle whose s i z e is dstermined by the value of HEIGHT. The s i z e of the rectangle is the same f o r a l l characters involved i n a given c a l l to SYMBOL. The value of (XLLHC,YUHC) gives the coordinates of the lwer left-hand corner of the rec- tangle associated with the f i r s t character t o be plot ted.

HEIGHT - The height of the characters ( in inches). The width of each character , f o r the purposes of determining t h e length of a plot ted character s t r ing , is 0.8*HEIGHT.

BCD - An array containing the character s t r i n g t o be plot ted.

ORIENT - The o r ien ta t ion a t which the s t r i n g is t o be p lot ted , measured CCW i n degrees from the +X axis.

NCHAR - The number of characters t o be plot ted. I f NCHAR is less than zero, one of a series of p lo t t ing symbols is d r a m centered on the point given by (XUHC,YLLEIC). Fi f teen symbols a r e avai lable , and the one draw. is determined by the absolute value of RCHAR (taken modulo 15) according t9:

- N C W Plo t t ing Symbol

1 square

2 c i r c l e

3 t r i a n g l e

4 cross ("plus" sign)

5 c ross ("Xt')

6 diamond

7 t i l t e d hourglass

8 upside-down teepee

9 z 10 Y

11 lozenge

12 a s t e r i s k (comb. of 4 L 5 )

13 hourglaus

14 v e r t i c a l l i n e

15 s t a r

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The s tandard cha rac t e r set, a s represented by the symbols on the 029 keyboard, is a v a i l a b l e through SYMBOL, with the except ion of t he follow- ing nine symbols: -,(,',@,7,&,~,#,0-8-2.

SUBROUTINE PLOTS (LUN)

PLOTS performs a l l of t he necessary i n i t i a l i z a t i o n f o r t he p l o t t i n g software. I t should be c a l l e d p r i o r t o c a l l i n g any o t h e r r o u t i n e i n t he package.

LUN - Logical u n i t number. I n a d d i t i o n t o t r ansmi t t i ng t h i s infor- mation t o t h e p l o t t i n g rou t ines , a t ape of t h i s number must be declared I n the u s e r ' s PROGRAM statement.

SUBROUTINE RSTR (IARG )

RSTR genera tes the c a l l CALL PLOT(0.,0.,6) i n o rde r t o c l e a r t h e plot- t i n g bu f f e r s and move t o a new page.

1-QRC - A dummy argument; i t is ignored.

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SUBROUTINE L I N A X S ( X O , Y O , X ~ , P ~ ~ L A B S I Z , W H I C H , N T I C , N L ~ , NDIGKT,NLABEL,LABEL)

LINAXS p l o t s and l a b e l s a l i n e a r a x i s .

XO - X coordinate of t h e left-hand edge of t h e p l o t i n inches.

YO - Y coordina te of t h e lower edge of t he p l o t i n inches.

X 1 - X coordinate of t he right-hand edge of t he p l o t i n inches.

Y 1 - Y coord ina te of t he upper edge of t he p l o t i n inches.

LABSIZ - (REAL) S i z e of the l a b e l s i n inches,

WHICH - (INTEGER) Ind ica t e s whether a ho r i zon ta l o r v e r t i c a l a x i s i s t o be p lo t ted :

WHICH = +1 v e r t i c a l = -1 hor i zon ta l

NTIC - Number of t i c k marks, including one a t t he end of t h e ax is . This is a l so , t he re fo re t he number of i n t e r v a l s i n t o which the t i c k marks d iv ide the a x i s .

NLFREQ - Frequency wi th which t i c k marks a r e t o be labeled.

VAL0 - Value of t he a x i s v a r i a b l e a t the beginning of t he ax i s .

VALMAX - Value of t h e a x i s v a r i a b l e a t the end of the ax i s .

NDIGIT - Number of s i g n i f i c a n t d i g i t s t o be used i n wr i t i ng t i c k mark l abe l s .

NLABEL - Number of cha rac t e r s i n a x i s l a b e l .

LABEL - Array containing the a x i s l a b e l .

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SUBROUTINE NUMBER(XLLHC,YUHC,HEIGHT,A,ORIENT,N)

NUMBER converts a number t o its EBCDIC representat ion and p l o t s it.

XLLHC,YLLHC - The coordinates i n fnches of the lower left-hand corner of the character s t r i n g t o be plot ted. (See the write-up f o r SYMBOL f o r a more complete expla2ation.)

HEIGHT - The height i n inches of the number on the p lot .

A - The number which is t o be converted and plot ted; is considered t o be an a r ray i f N is a FORMAT.

ORIENT - The o r ien ta t ion a t which he number is t o be plot ted.

- If the absolute value of N is less than 20, then the value of N is the number of decimal places t o be included. I f the absolute value of N is not less than 20, then N is assumed t o be an ar ray containing the FORMAT with which the number(s) i n A a r e t o be plot ted. I f N contains a format, then the element of the ar ray following the end of the format must contain a l l EBCDIC blanks, and the next word must contain the number of values i n the ar ray A which a r e t o be writ ten. The character s t r i n g generated by the format must be no more than 1000 characters long and must be terminated by an "@I'

symbol.

If HEIGHT is l e s s than zero, (XUHC,YLLHC) is assumed t o specify the

lower right-hand corner of the l a s t character t o be plot ted.

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Appendix C

LISTING OF PROGRAM SOURCE CODE FOR THE F'LEET ACCOUNTING MODULE

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C C C C C C C C C C C C ( U w D 1 U I U I t * . " w L U U I U I U U t m s m . r . * a S r C a , R

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2 - 0 C C .-- c u e m a > = a .e O L ' U C e.3 - * & =

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Q h . C C C C C C C C C C C C C C C t e C C C C C * C C C C C C C C C C C C C C C C C C C C C C b I-++ CC C C b C C C C N ulul W l u u w U 1 U I W W W V I U J U I I U U I U ~ U I I Y IUY'U1WYlUDtUUI W Y I U I W W U i I U W Y l W I Y I U W W Y ~ U ' U t W W W W W W W U I l U & Y ' U ' U I - a a = a r a ~ a ~ ~ d ~ r ~ r ( ~ c n r e r a a r r ~ c ~ r c r . c c c c m c r m c m r r c r r r r r c a a r r r r r e r r *, . . - - L

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- a a * 0 -

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V t - C V V V V W Y L W V Y Y V w w Y V v Y r V V V V V I V V Y Y ~ W ~ V V I W v W Y W V V ~ ~ ~ ~ ~ V U Y V V Y C w b - t Y C C L C L ~ C C C C C C L L L C C C L C C C C C C C C L F C L c c C C E C C C C C C C C C L C L C C C c c c e c c C C C C C ~ C ~ ~ ~ ~ C ~ C C C C O P F C ~ C C C C C ~ C C C ~ ~ C C ~ C ~ C ~ ~ ~ C ~ ~ ~ ~ ~ ~ ~ ~ r c r c r c ~ L T X Z S S S ~ r ~ s s x x x a t r t r ~ r f r x ~ a x ~ r ~ r r r r ~ r a r ~ r ~ ~ ~ ~ r t x ~ ~ r t r x x t

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- > - .- .)a Q -Q C -.*-

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e L a 'U 0

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.+ C I t . 1' LI L . ' IU ( Y " 4 I U l 1 L) &I*.& Y I 1 .U I I b ' l ' I I ' U ' U * l L ' I 1 I UI U* I 1 LL.W UIU, 'II*I. I U I I . - O ~ ~ O O O U O O o m o o o o ~ ~ n n o o s e e o a o o o c o s o o o m C - ~ l - I o d I a I O Z I 1 - 1 1 1 1 I 4 4 1 I 1 1 Q a . I . a - a a ~ rv f 2 T T T f T Y t Y Y T T Y T r Y Y + Y Z r r T Y f 7 7 7 T 7 Y X f r f - V W Y I C - c V I ) ( ~ V Y V ~ Y I W V * V I W ~ Y . Y Y Y V V Y W U ~ ~ ~ ~ ~ V Y ~ , Y ~ u

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9 ccc c c c c c c c c c c c c c c c c c c C C C C Or . C C O C , C C t C l C C @ C O - C O

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A p p e n d i x D

LISTING OF PROGRAM SOURCE CODE FOR THE AIRFRAME WWUFACTURER MODULE

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S Z 2 t O O C C C C C )

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d a u d . r e d U Y I C l w a O F U a e n P O L

-q: eary NU - a n O" - Y C U1 O U L L = w VIC C b C - 1 CIO r *a r - - a 0 - 0 nJ* m - C I - u - d ILE X V et vc k r V C ur a -,I UI* x o r w

C z z Z C Clccc C- V cnv Y r Z Z Z C W Y ~ wr r x t x r c r C c c e u

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? : - z : . t z : e - - Y I * C _ r i u i C C C . L C . - 2 0 - 0 . e l * C C ~ C E O O e V C ) Y U O U C

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C C C C C C C C b C C C C C C C C C C . C C C C C C C C C C t C C C Z Z Z T T 7 Z Z T 7 7 Z Z 7 X Z Z 7 7 Z Z f t Z Z 7 f Z Z T 7 7 Z 1 - 4 - 4 - - * e - - - - - - - . * * a a * * a a I - - - - * - - d d d d d d d d d d d d d d d d d d d d d - d d d d d d d d d d d a a a n a a a ~ ~ n ~ a a a a a a ~ ~ c n a a a a a o ~ a a o ~ a

C C C C C C C C C C C

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C e = C - C C e c C * c c c ~ c c c c t - c c e c c c c c c c t c c c c c c c c c c c .cc c c c c c c c c c c c c c 7 - 7 Z 7 Z Z 7 7 Z Z 7 2 Z t I 7 Z f 7 Z Z Z 2 2 2 2 2 Z Z t Z 7 7 Z 5 7 Z Z t Z P Z Z 7 Z Z 7 Z 7 7 ~ ? Z 7 Z Z

r. . . . - - * - . - 4 * Q - - - * a - 4 - - - * 4 - - - a e - * r a a - - - a - e - - a*-.- * - - - * * - - = *

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C C C C C C C C C C C C C C C C C C C C C C C C C C Y Z Z Z 7 7 Z . - 7 = 7 2 7 Z J 2 Z x 7 7 Z X Z T Z 7 - = I m I I I * * a C I I I I - a * - s - a a I - Q d44dd-1- -1-1ddddddd-1 -1ddddd- d d a a a n n o ~ a a a n a ~ n n a n a n a a a a a a a

C W z m e r r Y Y l 0

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o x - x - a n a . * ' U C + - a + -

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L.. 0

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L - L - W Z n u . C x r c 2 - C ~ C . o - 0 -- w - T a t r t u # T O W = a a .- w 2 I W U U C L C C a d - - a a - a k w u a ~ - I. u ~ ~ ~ u t ~ u u ~ u - l c x . c l a l b C C C C C c C Z a - - c - o - 3 a

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Y ) ( Y ~ I ( Y W V I W U ~ I ~ ~ Y ( Y Y U ~ I ~ U ) W ( Y Y . ~ ~ ~ V ~ U I U uaruwu ~ ~ W I Y ~ Y ~ V ~ ~ U ~ ( Y L ~ ~ Y ~ ~ U ~ ~ W Y . - U ~ ~ Y ' U ~ ~ ~ W U ) ~ ~ I ~ I ~ ~ W ~ ~ L I ' v ' ," .C.C V " ' L ' c V C C C L I S C L O C C . C . I * < ' C C . C C ' C ' C C t * C . C I . C ' L ' U C U L ' C ' C ' ( . ' C c c : 1 : I . . C ' C ' C L . " C ' C ' C C .-C . - C C I L C r L . - L - L L C C . V I n L V I - L C C L L * L L L C C-- - * - - -L - C C L * ---- ---- - ~ O P O O O L . O P O O D D m n o o o a m a o o a u e e o o o e o o e o a u a o a o o a n o n a n e o o o o e o m o c a a a ~ ~ a a ~ ~ ~ a ~ ~ a a ~ ~ ~ ~ ~ a a a n ~ e ~ ~ a a ~ P Q O ~ a a o o a a & n o ~ a n a a a a a a m & e m N C . C ' L ' F C U V C ' C L ' C * U C ' C ' U C ' C . C C V C L . C 7 U C . V C . U C . L ' L ' C ' C ' V < C ' U C ' U C ' V U C ' V W U I . ' L ' C VL 'C C C V L C'L' . . - - - . . - - * - 4 * - - * a * * a * * - a - - a a - - - - a . . - a - - a - - a - - a * - - - - a * -

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- C w C 4 C I - 3 5 s - 2 c 4 a a- Y a t w u UI I C U . W C r Z E r w . r CIC " C C C C

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v L 0 0 O O O P U ( C o m u a ~ o ~ ~ m ~ ~ o w a e h v ~ k a o a a d o 0 0 ( C O D O O W O 1 f f o . o w ~ a o a 0 m f f a c 6 o n a ~ ~ a ~ n a o a r a r ~ a r r a r ~ a ~ r . r ~ r a ~ o ~ r a ~ n o a a o r n o a r o o r n o n r a o o - C C C C C C C C C C C C C C C C ~ C C . C C C C C C ' C ~ C C C I - C C C C C C C C C C t C C C C C C C C C C C C C C v * & r w u w r . y , w w v ~ n n w ~ n ~ n w w v , c n v , r ~ ~ n y l n n ~ n r w v b - w r v , r w v n v r u u r w r m u I r w m v N r ~ e c c c o r r c c r c r c c c c e c c r o r e c o o ~ c c r o o o c c o c c c c c o c o o c e r r a c c r a ~ - U C V C C U U L ' C V C ' U U U U U U U C ' U U U V U O Y U U U V U U U U U U C I C ' U U C V L ' V U V L C V U U U V V V *

. Y c. 0 0

I- * + . N a l N

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4 u k r N U . L r l - . C mU C U N Y 0 L u r n r o e c n ~ C N - a NU>

L Z . C N d 4

2 W n l ' U N Z d Y . Z . a . d W .€

LY r y n r u . l C r m - LL a

.v .I- *. C * C N W O 3 m U t Q C - r ( W t C b 3 l U r e - . - Y Z L Y e e I G a N

c N 4 r W l t O 0 m . x u o t - a - c a m 4 h 4 t e e ~ ~ = a u , ~

4 C Y C o a - O m = & u a o a ~ r r

4 * b - w @ r ur o m 4 (C L ~ Z 5 Z ~ d Z W C C X

I I + n m - w l ( f h a C

C C Z Z V d * d d C r r m r o r d t a m

o w d a - z t u ~ r m r r C, a u r c t = s u - c ~ e t

o v n w c u n a c r u : = ~ ~ $ E ; g ~ ~ g E h H r ~ r r r f u T ~ r n z q f i e 4 - m r , J)N - . d I N H C I 4 N 4 * N r u . I . . * - . . B - * W h r a L I L L m I O I L o

%IUC , 060 3 3 0 - 0 0 - b *- d m 4 d - d 4 4- . u r * 4 . - . 4 4 * - 4 -

C . ~ ~ C ~ ~ T X ~ ~ T X X T T

0 C Y d . * @ r . r . r l d m d @ r ( o (re C . ~ O C - N C * ~ Q ; O C % Y L' c * U

$E *3 O V a L . r

NI- r C I *I-.- N . C . C . H r C C . Ylt u

IYC, r u d I E C m Y - 0 K t 4 -3 C I . . . . r u n

m e I- -.* n c C . C' r e .

::. . C - c. -7 e C C C 2- a> r a* . 0 . w

C w

a C P NC) V C C .

u - 0 r c n c C .* O C z n m .CW . ( am c e - 0 o I u U W 6 - 4 c Y U I O U I

H N 0 a !

e.Uc-• .I O C I w

r . l U N .

O r n Y C .N . * d I C . C

C O W 4 . . o a r . d

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-n I -

4- LC 'dm ~c -MI y rt- rv - Z d 3 ~ g E 3 t t * r C - r w u C r C h W , G r C

:EegE!:,,E " "7"'

- -- t M U ,

cY.;;: V ' S - O ~ x - W L . W C O I C s t - z r C wu t C L - O - U

*d 0 I e 3 - on, ruuuIu Z ;

I I

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Appendix E

LISTING OF PROGRAM SOURCE CODE FOR THE AIR CARRIER MODULE

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r r r YICb Y H * r a m d U I ULY) w o n

r . r C t r r Y U e a t UI r e a w O o C w m a W W I C O L W'JYIL HH

r u ~ a** uzn

t r YI r r r r r r -a a * I U I U I C I *YI r a w C l e * * H Y

a L I I I Y I I C n rn r r r r u a c c c r - U I H m W * a Z X e re- r IBawOmHm+.a

ro b r a 4 r nrl

r X X r r N r W - 2 r C C I W r m r % - >I rh U Y U W N -I r IJaYYU a x o u YI- 0 r- . r W U t * r C I a* 0-0 4 U O r L H H L ( L 400

UI rod 20 ncc r

4 u r r

o - N - ~

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L u I l M u Y w U w Y 1 w I Y Y w Y ~ Y ~ Y C Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y

w u u w ~ ~ ~ I Y u ~ u ~ ~ w m w ~ w 0 a.aaddaaadaaadA4adad N ICIIIIIIIIIaIIIIIaI

n o n ~ ~ ~ ~ o n ~ a a o o n a n n n * 0

0 Y) x U 4 Y) I

n LI

C w L n a YL V n a I

a .I( C r 3

u l * -1 N U - 0 0 C

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SU

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CA

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r W e r ry Y r

0" r U He Y C rn -3 V X

d I - O C

:3 4 a - * C Y

"Uff rn a d Y n I on= o u r aoC

- 4 x n w v m n

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*YCC (YO -+ e n . . e S . m * c * 0 LS;;S:: - l ) r r r ~ w

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0 d Y U a t 0 4 r-r

0- C O O U d I u r r * 1 4 W U U 000

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x C

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a CI " -1 n - a c. I v C m . a m 0 U

n m d . b

n C t m U 0 - 2 U m u l

r u U n r I o * u m - b H - m - t C u r - a n U Y N Y)n Y H O r ..UU*C. H 0 - nZT3Zm:

L W Z O W U o C a U X O U O Una I C N * a O I - C l n u r U C

W Y ~ U I O O O r r o a a a N U I ~ c W U O O O U 4 O I L I t 0 2 0 . O O c - d d a O o r 'Ca * a . r C U U o a - a r d X - r a w n - C a C I A r S r Z w C a m Y U Y O - r d u d Y Y m Y A Y U U Y

c i 40 u+ * - HI.

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n o a - u - r + Y m Y L 0- r w + r r w l C L - C b r C a w -Y)

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2 m a

m * a 3! ;;;;;=: . * a

-0 -4 Y Y Y

* - O O O * oaddd-

0- C C C H ~ 3 - 0 W L W U

r Y t . u r m a #

t --- --2 L - w H n U I am rnuaoane* - m a 3 = 3 a a e

b o o ~ c o a ~ d t ' C b m C # Y ) YIP--.cu*. W r - a # - 0 a W I N a** nY)=td V C

r r r t w v l f v r t a . IC ICC-HUCY U C YW.*.I I - w %Om- a*1-1u. 0 0 U U m U U o . I e o m a o e b e

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u o n s m U Z C * X I Y O ,?f*: -: a r c - rim e r I r X m X W l r 0- u r u r u r c t * I I O r n l O t ea .* W Y ~ ~ A ~ I U d r ~ u Y u I U W m w r

a * *.-a I- I r a - I r O C I l Y I UIwYImYIm --*I L . . . r L u b r C m I = t Z U H L U O C * C Y C I Y - 0 I Y HUnUnUauu

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Appendix F

COSMIC SOFTWARE SUBMITTAL INFORMATION

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Appendix F

COSMIC SOFTWARE SUBMITTAL INFORMATION

Abstract

The Analysis of the Benefi ts and Costs of Aeronautical Research and

Technology (ABC-ART) models have been developed by NASA f o r use i n analyz-

ing the economic f e a s i b i l i t y of applying advanced aeronautical technology

t o f u t u r e c i v i l a i r c r a f t . The methodology is composed of three major modules:

F lee t Accounting Module, Airframe Manufacturer Module, and A i r Car r i e r Module.

The Flee t Accounting Eodule i s used t o est imate the number of new a i r c r a f t

required a s a function of time to meet demand. This est imation is based

primarily upon the expected retirement age of ex i s t ing a i r c r a f t and the

expected change i n revenue passenger miles demanded. Fuel consumption

est imates a r e a l so generated by t h i s module. The Airframe Manufacturer

Module is used to analyze the f e a s i b i l i t y of manufacturing the new

a i r c r a f t demanded. The module includes log ic f o r production scheduling and

estimating manufacturing costs . For a series of a i r c r a f t s e l l i n g pr ices ,

a cash flow analys is is performed and a r a t e of r e tu rn on investment i s

calculated. The A i r Carr ier Module provides a too l f o r analyzing the

f inanc ia i f e a s i b i l i t y of an a i r l i n e purchasing and operating the new a i r -

c r a f t . This module includes a methodology f o r computing the a i r c a r r i e r

d i r e c t and ind i rec t operating cos t s , performing a cash flow analys is , and

estimating the in te rna l r a t e of r e tu rn on investment f o r a s e t of a i r -

c r a f t purchase prices.

The ABC-ART models a r e exercised i n two d i s t i n c t job s teps . The Flee t

Accounting Module and Airframe Manufacturer Module a r e run i n one job step.

The A i r Carr ier Module is run i n a second job s tep . The modules a r e

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designed f o r batch processing. Hardware requirements inc lude a card

reader , a p r i n t e r , and d i s k s torage . I n addi t ion , p l o t t e r output is

generated by t h e F l e e t Accounting Module. The software is c u r r e n t l y

programmed f o r a ZETA 230 p l o t t e r . The models have been run of a CDC 7600

with t h e SCOPE 2.1.3 opera t ing system. CPU time is very modest f o r e i t h e r

job s tep . However, core requirements a r e s u b s t a n t i a l . The f i r s t job

s t e p r equ i r e s 132K o c t a l words, t he second r equ i r e s 154K o c t a l words

small core memory p lus 144K o c t a l words of l a r g e core memory.

Method of Solu t ion

The methodology embedded i n the ABC-ART models is described i n

d e t a i l i n Volume I of t h i s r epo r t (NASA CR-152278). The methodology f o r

t he F lee t Accounting, Airframe Manufacturer, and A i r Ca r r i e r Modules a r e

described i n Sect ions 11, 111, and I V , respec t ive ly .

Computer Configuration Required

The ABC-ART models have been run on the NASA AMES CDC 7600, with the

SCOPE 2.1.3 opera t ing system. The only required input device is a card

reader. Required output devices inc lude a p r i n t e r , a p l o t t e r , and d i s k

s torage. The job s t e p which d e r c i s e s the F lee t Accounting and Airframe

Manufacarer Modules requi res a p r i n t e r , a p l o t t e r (software i s provided

f o r the ZETA 230 p l o t t e r ) , and four output d i s k f i l e s , two f o r s to rage of

d a t a generated f o r t h e p l o t t e r and two f o r temporary s torage of input data .

The job s t e p t h a t exe rc i se s t he A i r Ca r r i e r Module r equ i r e s only a p r i n t e r

and a card reader .

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Memory Required

On the CDC 7600 t h e r e a r e two types of memory, small co re memory (SCM)

* and l a r g e co re memory (LCM) . The F l e e t Accounting and Airframe Manufacturer

Modules r equ i r e 132K o c t a l words of SCM and no LCM. The A i r C a r r i e r Nodule

r equ i r e s 154K o c t a l words of SCM and 144K Words of LCM t o run. Var iab les

were placed i n LCM using the LEVEL 2 conversion f o r t h e CDC 7600.

Source Lanqu*

The ABC-ART models a r e programmed i n CDC FORTRAN extended 4 language.

The re fe rence manual f o r t h i s language is CDC Publ ica t ion Number 84000009.

The ZETA 230 p l o t t e r sof tware is w r i t t e n i n t he same language, except f o r

a s i n g l e COMPASS r o u t i n e ( l e s s than 1% of the code). COMPASS can be com-

p i l ed using t h e CDC FORTRAN compiler.

User I n s t r u c t i o n s

I n s t r u c t i o n s f o r use of ABC-ART models a r e provided i n Volume I,

Sec t ion V of t h i s r e p o r t where a sample run of t h e models is descr ibed.

Implementation I n s t r u c t i o n s

The sof tware package is being submitted i n t he f i v e d a t a s e t s . Each

d a t a set c o n s i s t s of a s i n g l e tape f i l e except f o r t h e f i f t h d a t a set,

which is composed of fou r tape f i l e s . These f i l e s a r e described below:

t On t h e U S A Ames computer system, l 6 O K o c t a l wards of SCY and 1,200K o c t a l works of LCM a r e ava i lab le .

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Data S e t s Tape F i l e Contents

1 1 FORTRAN source code f o r the F l e e t Accounting and Airframe Manufacturer Modules ( see Appendices C and D).

2 FORTRAN and COMPASS source code f o r t h e ZETA 230 p l o t t e r software.

3 FORTRAN source code f o r t h e A i r C a r r i e r Module ( see Appendix E).

Data input f o r t h e sample run of t h e A i r Carrier Module ( see Volume I, Table 41).

5 5,6,7,8 Data input f o r sample run of t h e F l e e t Accounting and Airframe Manufacturer Modules (see Volume I, Table 40).

The tape conta ining these f i l e s i s a n unlabeled, S t r a c k tape i n the

EBCDIC charac te r s e t with a dens i ty of 1600 BPI. The l o g i c a l records a r e

i n card image format, 80 charac te r s i n l eng th with no blocking. The tape

was w r i t t e n on a CDC 7600 computer i n SCOPE s t ranger format (i.e., F-S).

No job con t ro l language i s included i n any of t h e f i l e s .

Program Timinq

The CPU time required t o run the ABC-ART models is q u i t e modest. It

w i l l vary with t h e problem analyzed, the main f a c t o r being the number of

new a i r c r a f t types. The sample run of t h e ABC-ART models, described i n

Volume I, Sect ion V, took 22 and 4 CPU seconds f o r t h e F l e e t Accounting

and Airframe Manufacturer modules ar?d A i r Carrier K d u l e , respect ively .

This time includes 5 and 3 CPU seconds, r espec t ive ly , f o r compilation.

Accuracy of Resul ts

The ABC-ART system does not conta in mathematical o r s t a t i s t i c a l rou t ines

t h a t a r e very s e n s i t i v e t o vord s i z e . S ing le p rec i s ion ca lcu la t iona on t h e

CDC 7600 use a 60-bit word which provides a high degree o i accuracy i n

computed r e s u l t s .

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Sample Input and Output

Volume I of t h i s r epo r t provides sample input and r e s u l t i n g output.

I n Sec t ion V, t h e sample problem is descr ibed, inc lud ing a l i s t i n g of t h e

card input . Excerpts from the r e su l t i rk? pr in ted and p l o t t e d ou tput f o r

t h e F l e e t Accounting, Airframe Manufacturer and A i r C a r r i e r Modules a r e

provided i n Sec t ions 11, 111, and I V , r espec t ive ly .

Flowcharts

Flowcharts nf t he l o g i c of each o f the rou t ines i n t he ABC-ART models

have been provided i n Volume I of t h i s r epo r t . Flowcilarts f o r t he F l ee t

Accounting, Airframe Manufacturer, av . J A i r C a r r i e r Modules a r e provided i n

Sect ions 11, 111, and IV, respec t ive ly .

Program L i s t i n g

L i s t i n g s of t h e FORTRAN code f o r the ABC-ART models a r e provided i n

Volume I1 of t h i s repor t . Program l i s t i n g s f o r t he F l e e t Accounting, A i r -

frame Manufacturer, and A i r Ca r r i e r Modules a r e provided i n Appendices C,

D, and E, r espec t ive ly .