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(lASA-TI-X-729C1) ZAlUEiN 1E ANL SATUFN 5 N76- 13 156 CCIFUTEF FkCGfiAFS, SCHYAPE Status 6c~ort (tiASA) 78 F BC s5.C~ CICI 221: t t I i g I 5 * f , <-* '7 ~ - \ TR-612 - Revision 13 I I July 5, 1972 , - 1' . CHECKOUT AUTOMATION AND PROGRAMMING OFFICE * JOHN F. KENNEDY . . KSC FORM 16-12 (4/'91 LV-C I' *_. - .- ., - I 1 - . , / .-. - -4 - -y:- - - I SPACE CENTER I I i I I / \@+ - 1 / .-J r j ' ~ -' SATURN I6 AND SATURN V COMPUTER PROGRAMS, SOFTWARE STATUS REPORT Ill I I I I I
79

JOHN F. KENNEDY SPACE CENTER

Jan 20, 2023

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Page 1: JOHN F. KENNEDY SPACE CENTER

( l A S A - T I - X - 7 2 9 C 1 ) Z A l U E i N 1E A N L S A T U F N 5 N76- 13 156 CCIFUTEF F k C G f i A F S , S C H Y A P E S t a t u s 6 c ~ o r t (tiASA) 78 F BC s 5 . C ~

CICI 221:

t t I i g

I

5 * f , < - * '7

~ - \

T R - 6 1 2 - Revision 13 I

I July 5 , 1972 ,

- 1' .

CHECKOUT AUTOMATION AND PROGRAMMING OFFICE

*

JOHN F. KENNEDY

. .

K S C F O R M 16-12 (4 / '91

LV-C

I '

* _ . - .- ., - I 1-

. ,

/

. - . - -4 -

-y:- -

-

I

SPACE CENTER I I i I

I

/ \@+ -

1 / .-J r j ' ~ -'

SATURN I6 AND SATURN V COMPUTER PROGRAMS, SOFTWARE STATUS REPORT

Ill I I

I

I

I

Page 2: JOHN F. KENNEDY SPACE CENTER

JOHN F. KENNEDY SPACE CENTER, NASA

T R - 6 1 2 Revision 13

SATURN IB AND SATURN V COMPUTER PROGRAMS, SOFTWARE STATUS REPORT

by

Checkout Automation 2nd Programming Gffice

LAUNCH VEHICLE OPERATIONS

July 5, 1 9 7 2 i

Page 3: JOHN F. KENNEDY SPACE CENTER

JOHN F. KENNEDY SPAZE CENTER, NASA

TR-612 Revision 1 3

SATURN IB AND SATURN V COMPUTER PROGRAMS, SOFTWARE STATUS REPORT

Checkout Automation and Programming Office

ABSTRACT

This report i s prepared by the Checkout Auton~ation and Programming Off ice (LV-CAP) and is intended to present to NASA elements and Saturn Stage Contractors the progress and development of a l l requested Saturn IB and Saturn V Computer Programs.

Page 4: JOHN F. KENNEDY SPACE CENTER

TABLE OF CONTENTS

Section . Title

INTRODUCTION

Page .

I ON-LINE PROGRAMS

1-1 General . . . . . . . . . . . . . . . . . . . . . . . 1-1 1-2 F0rms . . . . . . . . . . . . . . . . . . . . . . . 1-1

I I OFF-LINE PROGRAMS

L IST OF TABLES

Table Ti t le . . . . . . . . Saturn I B Operating System and Test Programs

. . . . . . . . . . . . Saturn I B Major Test Program Matrix Other Saturn I B Systems Programs . . . . . . - . . . . . . . Saturn V Operating System and Test Programs . . . . . . . . Saturn V Major Test Program Matrix . . . . . . . . . . . . . Other Saturn V Operating Systems and Test Programs . . . . Saturn IB/V Operational DEE -6 Programs . . . . . . . . . Saturn V DDP-224 Display OPSY Programs . . . . . . . . . Saturn V Display Descriptions . . . . . . . . . . . . . . . Saturn V Per~nanently Masked MDls . . . . . . . . . . . . . Machine Language Subroutines . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . ATOLL Sub Programs RCA-11OA Supplemental Diagnostic Programs . . . . . . . RCA-1lOA Supplemental Ut i l i ty Programs . . . . . . . . . RCA-11OA Supplemental Postprocessing Programs . . . . .

. . . . . . . . . . . . . . DDP-224 Supplemental Programs DEE-6C/E Supplemental Diagnostic Programs . . . . . . . . DEE-6C/E Supplemental Ut i l i ty and Postprocessing

. . . . . . . . . . . . . . . . . . . . . . . . . . . Programs

Page .

Page 5: JOHN F. KENNEDY SPACE CENTER

INTRODUCTION

The Software Status Report (Saturn IB and Saturn V Computer Progran~s) i s prepared quarterly by the Checkout Automation and Programniing Office 'LV-CAP), and i s intended to present to NASA elements and Saturn Stage Contractors current information i Saturn I B and Sal urn V Computer Programs. The informa- t ion contained in this report was val id as of approximately 15 days prior to i t s publication date.

The report i s divided into two sections. Section I conta iz i on-line, ooerating system, and tes t pro- grams and on-line display descriptions. Section II contsills the o f f - l ~ne programs, and other supplemental programs .

A l l programs are l isted in tabsldr form, and those llavirig an Internal Variable (IVAR) are arranged alphanumerical ly wi thin eacll table. The f i rst character of the IVAR represents one o f the following:

B.. S-IClfS-IB Stage Propellants C.. F l ight Cot~trol D.. Diagnostics E.. S-IVB A T O L L (SIB) F . . F l i gh t Computer G . . P!atfortn (Gu~dance) I . . 18 Integration ATOLL J.. A T O L L Training Progrnrn K.. I U Stage A T O L L (V) L.. I U Stage ATOLL (SIB) M.. Measurements

N.. Networks 0.. S-IB Stage A T O L L P.. S- l l Stage Propellants Q.. S- l l Stage A T O L L T.. Telemetry U.. Ut i l i t y V.. Saturr~ V Integra!ion A T O L L W.. S-IC Stage A T O L L X.. S-IVB Stagc A T O L L (V) Z . . Postprocessing

The second character o f the IVAR (ii on-line programs) closely represents the type of computer program described, or adds def~n i t ion to the i l rs t IVAR cl~aractcr. They are as follows:

A.. A T O L L Language Progran; T . . Test E . . Function Executor U.. U t i I ~ t y M.. A T O L L Machine Language Subroutine X . . ATOLL Subroutine S . . Stand-Alone, or Remote Z . . ATOLL' Language Sub Program

The third and fourth characters of the IV4Rs tnay l!e letters or numbers

Block diagram of the L C - 3 9 Display System and Colnputer Complex i s i l lustrated in Figure 1.

The Saturn Display System (Figure I) IS comprised of 1 5 consoles configured as follows:

Console No. Rack Position Primary Functlon Resp. Org . 1 Cornputer Room System I r i ~ t ~ a l ~ z a t i o n arid Hardware Status I B M

2 B E 8 Software Systeni Status IBM/NASA

3 B E 2 4 Propellant Monitoring TBC

4 B D l O F l i gh t Control Syste~l l T2st and Status I B M

5 B D 2 3 S-IC Swing Arin and T a l l Fervice Mast T e s t i i g & Status TBC

6 BCS Dlatforrr~ Posit ioning atid Monitoring lBlVl

7 B C 1 2 F l i gh t Computer Test, Status, and Operations I B M

8 BE 2 Measuring Systern Control I B M

9 B B 1 2 EDS Test ing I B M

10 B B 2 0 S-IVB System Status MDAC

11 B B 2 6 S-IVB Automatic Testiny MDAC

1 2 B A 5 Linkage C ~ n t r o l for lntegrdted Test ing and S-IC Status TBC

Page 6: JOHN F. KENNEDY SPACE CENTER
Page 7: JOHN F. KENNEDY SPACE CENTER

Console NO. Rack Position -- Primary Function

12* BA5 Linkage Control for Integrated Testing

Resp. Org .

TBC

1 3 BA 1 4 S-IC Automatic Testing TBC

13* BA 14 NASA Operations Engineer (CLE S) NASA

1 4 B A 2 0 S-l l Mechanical Testing and Status NA R

14* B A 2 0 S-IB Mechanical Testing and Status CCSD

1 5 B A 2 6 S-l l Electrical Testing and Status NAR

15* B A 2 6 S-IB Electrical Testing and Status CCSD

Consoles 1, 2, and 9 are System Masters, and therefore can call or terminate any test program and issue discretes (MDOs).

Consoles 1, 3, 7 , 9, and 12 in the prime firing room may be drlven by a backup display computer, in the event the prime display systelii goes down.

*Firing Roorn *3 only (S-IB vehicles)

The responsible contractors are identlfled in the tables by mnelnonlc name, and the necessary liaison wlth the responsible contractors enqlneering organizations may be arranged ttirough tile respective Stage Autorriatiori Representatives.

Contractor Company Stage Automation Representative Telephone

BATC Boelng Atlantic Test Center J. Smith 8 6 7 - 6 5 6 5 CCSD Clirysler Corp Space D i v ~ s ~ o n H. Cdnrad 8 6 7 - 7 0 0 3 IBM Inter~iational Business Macl l l~ie R. Lindner 8 6 7 - 4 3 2 0 MDAC McDotinell Douglas Astronautics Co. H. Lanier 8 6 7 - 7 5 4 0 NAR North Aniericat~ Rockwell Q . Price 8 6 7 - 3 5 1 6

NOTE

Where any d~screpanc~cs or errors occur in the scope, format, or conte~:t, please notify:

John B. Thompson, Jr., LV-CAP-A, 8 6 7 - 3 7 5 9 LV-CAP-B, 8 6 7 - 3 7 8 7 (Section I, for on-line programs) (Section II, for off-line programs)

v i i

Page 8: JOHN F. KENNEDY SPACE CENTER

SECTION I ON-LINE PROGRAMS

1-1 GENERAL

This section l ists a l l the on-line programs for Saturn 18 and Saturn V launch vehicles. Information contained i n the tabular portion includes IVARs or Call Numbers, Program Titles, Functional Descriptions, hardware/software Interfaces, and program Status (release date, vehicle effectivity, etc.). The fol low~ng tables appear in this section:

a. Table 1-1, Saturn IB Operating System and Test Programs; These pograms are used in performing Saturn IB vehicle testing operations.

b. Table 1-2, Saturn If3 Major Tesi Program Matrix; This table supplements Table 1-1 by showing which programs are used during major vehicle testing operations.

c. Table 1-3, Other Saturn IB Sy:tems Programs; These programs are run on launch complex hardware, but are not used in dircct support of vehicle testing.

d . iable 1-4, Saturn V Operating System and Test Programs; These programs are used i n performing Saturn V vehicle testing operations.

e. Table 1-5, Saturn V Major Test Program Matrix; This k b l e supple~~lerlts Table 1-4 by showing which pograms are used durinq major vehicle testing operations.

f. Table 1-6, Other Sdturrl V Operatino Systems and Test Programs; Ttiese programs are run on launcti hardware, but are n.>t uced In o~rect support of vehicle testing.

g. Table 1-7, Saturn I B / V Operational DEE-6 Programs; These programs are used i n support of vehicle testimj operations.

h. Table 1-8, Saturn V DDP-224 Display OPSY Programs; These programs are the DDP-224 on-line and executive display OPSY programs.

i. Table 1-9, Saturn Display Descriptions; These descriptions coritain the display formats i n tne display description tape, which are used for communi-.ating between the DDP-224 Operations Display System and the Saturn Operating System.

1. Table 1-11), Saturn V Masked MDIs; These M31s are permanently masked i n the Saturn V Operating System.

k . Table 1-11, Mhchine Languaye Subroutines; Pri jv~de special purpose mach~ne language capability for ATOLL programs.

I . Table 1 -12 , ATOLL Sub Programs; Subprograms~which extend the capacity of the parent program. S-IB - Sub-Programs and "I" Sub-Programs not l isted i n Table 1-1 2. - 1-2 FORMS

Three basic KSC Forms are used to present the data for the on-line pograms; KSC Form 16-226, 16-225 , and 1 6 - 2 2 8 . An explanation of the significance of the headings and column titles, and guide- lines for interpreting the data contained in the tables are presented i n 1 -2 -1 through 1-2-3.

1 - 2 - 1 KSC Form 16-226 . This form i s used to present the Saturn 18/11 Operating System and Test Programs, Other Saturn IB/V Systems Programs, and the Saturn V DDP-224 Display OPSY Programs. The column headings, on the form, are as follows:

a. IVAR; The Internal Variable listing in alpha-numerical sequence. (Programs not assigned an IVAR w i l l be l isted at the end of each table under the designation of N/A.)

b. NASA Auth Element and Responsible Contractor; The mail code of the NASA agency (must be preceded by LV), and the mnemonic name of the responsible contractor.

c . Program Title and Function; The applicable program tit le, and a short description of its function.

Page 9: JOHN F. KENNEDY SPACE CENTER

d. Interface; Conlputer input/output systems are identif ied i n the column t i t les . An "X" placed in the colurnn under Interface, i n+i4 ates that the program uses that system, but does not imply that the program uses only the l isted systems (on .oe form). The abbreviations for the system function are as follows:

Abbreviation

analog DDAS CDC ISSUES MDO ISSUES SSEL PRINTER Dl SPLAY GM T

Systern Function

Input or Output Analog functions Digi tal Data Acquisit ion System Countdown Clock Issues Mobi le Launcher DO or AGCSC DOV l s s ~ i e s Switch Selector functions L ine Printer Display System Greenwich Mean Time

o . Status and/or Remarks; Used to present special status/remarks of applicable programs.

f. Auth. for Vehlcle No; W e n forma! duthorization by LU-CAP for use of a program occurs on a vehicle basis, the number(s1 of the vehicle(s1 for which the program i s authorized w i l l be entered in the colurnn.

1-2-2 KSC Form 1 6 - 2 2 5 . This torm i s used to l i s t the Sat~ l rn I B and Saturn V Major Test Programs, and the explanation of columr~ headings i s as follows:

a. IVAR; The Internal Variable l i s t ~ n g , in alpha-nrrmer~cal sequence. (Programs not assigned an IVAR, w i l l be l isted at the end of each table under the designation of N/A.)

b. Test Tit le; The Major Vehicle or Stage Test T i t les are l isted in these columris. An "X" placed under a test t i t l e siqriifles that the test program [nay be used for that test.

c. Remarks; Co~i ta ins special instructions applrcable to the lrsted IVAR, i f required.

1-2-3 KSC Frrni 1 6 - 2 2 8 . This form i s used to l ~ s t the Saturn V Drsplay Descriptions, and the explana- t ion of column headings i s as follows:

a. Display Desc. No.; Numerical sequence of DD numbers. Thece numbers serve to rdentrfy the DD requestpr, and the oumbers are assigned in blocks to each requestirlq agency. The number block assignments are as follows:

Requezting Organization DD NIIIIIIIE~S Cal l Numbers

NASA (KSC) NA F! MDAC IBM (KSC) IBM & NASA (MSFC) BA TC (Spares) CCSD

b. Call No.; These numbers identify the display location on the DO Tape, and are used by the console operator to ca l l the desired description.

c. Description; Identif ies the description by i ts formal t i t leland to note the part number or page number for description bearing identical t i t les.

d. Authorized for Vehicle; The applicable vehicle seria! nurnber(s1 are l isted i n the cclurnn heading, and an "Xu is placed under a given serial number to denote that the description i s authorized for use on that vehicle.

Page 10: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

IYT

ER

FA

CE

N

AS

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UT

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0

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. E

LE

ME

NT

AN

D

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R

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R

RE

SP

ON

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LE

-

PR

OC

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M T

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ON

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ND

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AC

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PR

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; C

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ly m

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20

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final

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for

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WE

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gram

Page 11: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

tinq

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

AUTM

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erif

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PR

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dis

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W a

ssoc

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etti

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fun

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T2O

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icle

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INS

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PS

ME

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by

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Page 12: JOHN F. KENNEDY SPACE CENTER

Tab

le 1-1 ..

Sat

urn

If3 O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

PR

OG

RA

M T

ITL

E &

FU

NC

TIO

N

lVA

R

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

C

ON

TR

AC

TC

R

GD

C-2

3

EA

PF

EA

P L

S-I

VB

PR

OP

ULS

!ON

CH

EC

KS

; C

heck

s th

e fu

nd

ion

and

tim

ing

of p

ropu

lsic

n vn

lves

,

( EAP

D

CD

C-2

3 M

DA

C

EA

PS

EA

PU

EA

PX

EA

SR

I MDA

C

auto

mai

cally

cal

ls N

TDR

to

cc

di

scre

te e

on

i

ng

. M

akes

fun

ctio

nal

chec

k /

of S

-IV

B p

ress

ure

switc

hes.

S-I

VB

PO

WE

R D

IST

RIB

UT

ION

; V

erifi

es a

po

wer

dis

trib

utio

n an

d co

~it

rol s

witc

hing

ci

rcui

ts,

for

vehi

cle

atid

ES

E.

Sub

Pro

gram

EZ

PD

; i

G3C-23

S-I

VB

PR

EP

S A

ND

FU

NC

TIO

NA

L;

Fun

ctio

nally

che

cks

S-I

VB

sys

tem

s re

quire

d to

S

ub P

rogr

am E

ZP

F

MD

AC

su

ppot

t ov

eral

l tes

ts t

hrou

gh F

RT

.

j I

!

GD

C-2

3 I 5-IV

f3

PA

NE

L L

AM

P S

EQ

UE

NC

ER

TE

ST

; P

rovi

ces

reri

iica

tio

~i of

int

erla

ce b

etw

een

i 1

/ X IX 1

M

DA

C

LCC

atid

pan

el la

mps

ope

rate

d by

LD

O's

. 1

1 S-IV

B P

OW

ER

SE

TUP

; P

rovi

des

a se

quen

tial

pow

er tu

rnon

and

tur

noff

for

the

vehi

cle

subs

yste

m a

nd s

tage

inte

grat

ed te

st.

GD

C-2

3 I

S-I

VB

PR

OP

ELL

AN

T U

TIL

IZA

TIO

N;

Pro

vide

s se

mia

utom

atic

mea

:is

(via

SG

CC

) to

FJ

DA

C

1 det

erm

ine

oper

atio

nal

stat

us o

f S

-IV

B s

tage

Pro

pella

nt U

tili

za

tio

~ (PU

) su

bsys

tem

. I

GD

C-2

3 1

S-I

VB

PO

YC

R T

RA

NS

FE

R;

Fun

ctio

nally

ver

ifie

r th

e S

-IV

B p

ower

tra

nsfe

r ci

rcui

try.

M

DA

C

I I

GD

C-2

3 ;

5-IV

B R

AN

GE

SA

FE

TY

FU

NC

TIO

NP

L T

ES

T;

Sem

iaut

om;l!

ical

ly

dete

rmili

es t

he

UD

AC

i op

erat

iona

l cap

abili

ty o

f cr

itic

al e

lem

ents

of t

he R

aocj

e S

afet

y S

ub

- em

.

i

AU

TH

. F

OR

V

EH

ICL

E

NO

.

-

20

5

thru

2

09

4..

Page 13: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

ting

Sys

tern

and

Tes

: P

mrn

ns

(C

ontin

tled!

EA

SS

WE

50

*FT

Bl

*FT

03

*FT

04

I NA

SA

AUT

H.

1 E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

I C

ON

TR

AC

TO

R I

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

GD

C-2

3 S

-IV

B S

WIT

CH

SE

LEC

TO

R R

ES

ET

; R

eset

s th

e S

-IV

B s

witc

h se

lect

or f

utic

tions

afte

r M

DA

C

an i

nput

has

bee

n m

ade.

IU/A

CC

ELE

RO

ME

TE

R

MO

NIT

OR

; S

cale

s an

d m

onito

rs t

he o

utpu

t fro

m t

he L

VW

; A

ccel

~ror

n-.t

er M

otlit

or P

rogr

arn.

LV

DC

TA

RG

ET

ING

DA

TA

TE

ST

; U

pdat

e ta

rget

~nf

orm

atio

n for

rend

ezvo

us m

iss~

ori

o

f S

kyla

b.

GD

C-3

2 LV

DC

/LV

DA

S

WIT

CH

SF

LEC

TO

R I

NT

ER

FA

CE

TE

ST

; P

rov~

des th

e c

ap

ab

~l~

ty

of

IBM

I ver

ifyin

g th

e LV

DC

inte

rfac

e w

ith

the

swit

ch s

elec

tors

.

GO

C-3

2 1 V

OC

/PO

WE

R

ON

-OFF

A

ND

/OR

R

ED

UN

DA

NC

Y T

ES

TS

; P

rovt

des

the

capa

biltt

y of

IS

M

appl

ying

or

rem

ovin

g po

wer

to

the

LV

DC

AV

DA

, ;n

d/or

pe

rform

s ch

ecki

ng f

unct

ions

.

GD

C-3

21

LVD

C/D

AT

A L

OA

D A

ND

/OR

V

ER

IFY

TE

ST

; P

rovr

des

tile

c~

pi~

tlit

y

of l

oa

d~

ng

dqta

iB

M

I in

to,

and/

or

veri

fyin

g da

ta w

ithin

, th

e LV

DC

mem

ory

from

a g

lver

, po

in!.

I IN

TE

RF

AC

E

I I

1

GD

C-3

2 L

VD

C/G

lMB

AL

AN

GLE

RE

AD

TE

ST

; O

utpu

ts :h

e gi

mba

l an

gle

stat

us,

utili

zrng

the

IBM

) Gim

bal A

ngle

Mon

itor

Pro

gram

in

the

LVD

C.

1 AU

TH.

FO

R

-1

ST

AT

US

AN

D

OR

RE

MA

RK

S

+

3 Z

L

NO

.

z4

1

a0

0

X

X

Link

ed b

y L

AP

S,

I E

AP

D

X

X

X,

Link

ed b

y IA

L-K

, I L

AS

S

X

X

i L~

nk

ed

by I

AL

K,

LAC

M,

LAP

G,

LAP

W,

LA

RT

1 LA

GC

, L

AP

G

GD

C-3

21

LVD

C/S

ELE

CT

OR

D

UM

P T

ES

T;

Con

iman

ds L

II~ p

rtnt

out

of L

VD

C m

emor

y se

ctor

. ?

:X

~X

IB

M

1 ,

, I

I/

~

II

;

GD

C-3

2 LV

DC

CO

RE

MA

P L

OA

D A

ND

/OR

P

RIN

T T

ES

T;

Ret

rieve

s til

e C

ore

Map

from

the

I x

,x

IBM

LV

GC

, st

ores

it

in t

he L

CC

, an

d p

rin

ts i

t on

the

LCC

lin

e p

rinte

r.

YT

10

/ GD

C-3

21

LVD

C/L

VD

A

LAD

DE

R O

UT

PU

T T

ES

T;

Exe

rcis

es t

he l

adde

rs t

o pr

ove

the

LV

DA

6s

IRM

!

stee

ring

com

man

d ca

pabi

lity.

I

YT

2O

I G

DC

-321

LV

DC

;LV

DA

S

ELF

-TE

ST

; P

erfo

rms

nti e

rror

che

ck o

f th

e LV

DA

.'LV

DC

, u

tili

z~n

g,

IBM

w

here

pra

ctic

al,

the

LV

DC

rout

ines

to

perfo

rm th

e er

ror

chec

king

. i

YT

23

G

DC

-321

LV

DC

iSE

CT

OR

SU

M C

HE

CK

; P

rovi

des

the

capa

biltt

y of

det

err!i

ttitri

g ~f

ally

spe

ctf~

ed

IBM

/

LVD

C m

emor

y se

ctor

lia

r a

valid

che

ck s

um.

ISC

FO

AM

16-

226

(RE

V.

5 6

9)

*MS

FC

Del

iver

ed P

roga

rn

Link

ed b

y IA

LK,

IAL

L,

!AT

S

Link

ed b

y L

AP

G

Link

ed b

y IA

LK

, L

AP

W

Link

ed b

y IA

LK

, IA

LL

, L

DF

C

Link

ed b

y IA

LK

,

j j LA

PW

xix

1 Linked

by I

AL

K,

LAC

M,

LAP

G,

LAP

W

Page 14: JOHN F. KENNEDY SPACE CENTER

Tab

le 1-1. S

atur

n IB

Ope

ratin

g S

yste

m a

nd T

est

Pro

gram

s (C

ontin

ued)

IV*R

*FT

25

*FT

27

*FT

31

*FT

33

*FT

35

*FT

37

*FT

42

WT

43

VT

45

*FT

47

?SC

FO

RM

*MS

FC

INT

LR

f AC

E

NA

SA

AU

TM.

CLE

ME

NT

AN

D

~ESP

ON

SIIL

E C

ON

TR

AC

TO

K

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

PROG

RAM

TIT

LE

6 F

UN

CTI

ON

-

LVB

C/L

VD

A D

ISC

RE

TE

IN

PU

l TE

ST;

Ver

ifies

that

the

LV

DC

can

pcr

perly

rea

d it

s di

scre

te i

nput

s.

SIM

ULA

TE

D F

LIG

HT

MO

NIT

OR

TE

ST;

M

onito

rs a

nd r

ecor

ds t

he e

vent

s re

sulti

ng

from

the

ope

ratio

n o

f the

Flig

ht S

imul

atio

n R

outin

e in

the

LVD

C.

LVO

C A

CC

ELE

RO

ME

TE

R P

ULS

E C

OU

NT

TES

T; E

rerc

ises

the

Acc

eler

omet

er

Pul

se C

ount

Rou

tine

of th

e LV

DC

to e

nsur

e fu

nctio

ning

of

the

acce

lero

met

er p

roce

ssor

as

soci

ated

with

the

ST

-12

4M

pla

tform

acc

eler

omet

ers.

LVD

C/L

VD

A D

ISC

RE

TE O

UTP

UT

TES

T; V

erifi

es t

hat

the

LVD

C d

iscr

ete

outp

uts

can

be s

et a

nd r

eset

.

LVD

C/L

VD

A D

DA

S T

ES

T,

AG

CS

/MLC

; V

erifi

es p

rope

r op

erat

ion

of t

he in

terf

ace

betw

een

the

LVD

C te

lem

etry

buf

fer

and

DD

AS

.

SIM

ULA

TE

D F

LIG

HT

INIT

IALI

ZE

; P

rovi

des

hard

war

e ch

ecks

arid

ind

icat

or w

ords

to

the

Sim

ulat

ed F

light

Mon

itor.

C

omm

ands

LV

DC

to th

e fo

llow

ing

mod

es:

a.

Pre

para

tion ~n la

unch

with

out

a pl

atfo

rm.

b.

Pre

para

tion

to l

aunc

h S

imul

ated

Fliy

lit w

ith a

pla

tform

.

AU

TII.

d ?

::

i c.

R

epea

tabl

e S

imul

ated

Flig

ht.

o

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

16-2

26 (R

EV

. 5/

69)

NO

.

ITA

TU

S A

ND

/OR

7

RE

MA

RK

S

ytnl

c~e

PR

EP

AR

E T

O L

AU

NC

H;

Pro

vide

s ha

rdw

are

chec

ks,

LVD

C i

nit.

ial~

zatio

n, an

d S

CC

in

itial

izat

ion

for

Flig

ht P

rogr

ams.

LVD

C C

OM

PU

TER

IN

TE

RF

AC

E U

NIT

TE

ST;

Ver

ifies

CIU

ope

:atio

n w

ithi

n th

e In

stru

men

t U

nit

Sys

tem

. T

est

Ope

ratio

n of

the

Gui

danc

e S

yste

m i

n a

ddre

ssin

g an

d re

ceiv

ing

data

from

:he

CIU

.

LVD

C C

OM

MA

ND

SY

ST

EM

TE

ST;

V

erifi

es c

omm

unic

atio

n at

bet

wee

n G

uida

nce

Com

man

d S

yste

m a

nd L

VD

A/L

VD

C.

Chec

ks

sign

al s

tren

gth

in G

uida

nce

Com

man

d R

ecei

ver a

nd D

igita

l D

ecod

er.

PR

EF

LIG

HT

CO

MM

AflO

TE

ST;

Com

man

ds th

e O

rbita

l R

outin

e of

the

Flig

ht

Pro

gram

to

enab

le c

omm

unic

atio

n w

ith t

he L

VD

C.

!%

0 2

4

Del

iver

ed P

rogr

am

X T z

g:

d5

LO

0

X

X X

20

6

thr~

20

9 / X X X X X

X X X X X X

X X X X X

Link

ed b

y LA

DO

, LA

GC

Link

ed b

y IA

TS

, LA

GC

Link

ed b

y IA

LK,

LA

ST

Link

ed b

y IA

LK

Link

ed b

y IA

ED

, L

AD

0

Link

ed b

y IA

LK,

LAP

W

Link

ed b

y IA

LK,

IAT

S,

LAP

G,

LAG

C,

LA

ST

Link

ed b

y IA

TS

Link

ed b

y IA

LK,

LA

SS

Link

ed b

y IA

LK,

IAL

L,

LAC

M,

LA

GL

Link

ed b

y IA

LK,

IAL

L,

LAC

M,

LAG

C

I X X X Y X X

X X X X X X

Page 15: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

0

h

O-

'

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

0

RLS

PO

NS

IBLE

U

¶

%

C

ON

TR

AC

TO

R

* *

W

w

GD

C-3

2 A

CC

ELE

RO

ME

TER

MO

NIT

OR

DIS

PLA

Y C

ON

TRO

L;

Dis

play

s op

tlons

for

and

IB

M

exec

utes

FE

50.

GD

C-3

2 LV

DC

STE

ER

ING

TE

ST;

C

omm

ands

LV

DC

to e

nter

gui

danc

e an

d co

ntro

l S

teer

ing

IBM

I Test

and

to r

etur

n LV

DC

to M

ode

Sor

t. II

II

GD

C-3

2 LV

DC

TE

LEM

ET

RY

TE

ST;

Com

man

ds th

e LV

DC

to e

nter

a te

lem

etry

tes

t ro

utin

e,

BM

I and

load

s an

inp

ut w

ord

to s

peci

fy th

e ra

te o

f tel

emet

ry.

IIII

I G

DC

-32

SIM

ULA

TE

D F

LIG

HT

PO

ST

PR

OC

ES

SO

R T

ES

T;

Pro

vide

s th

e ca

pabi

lity

of

IBM

1 proce

ssin

g th

e ra

w d

ata

gene

rate

d bj

the

ove

rall

Sim

ulat

ed F

light

Tes

t P

rogr

am.

GD

C-1

2 A

ZIM

UT

H P

OS

ITIO

NIN

G A

ND

MO

NIT

OR

; M

onito

rs th

e az

imut

h en

code

r fo

r dr

ift,

IBM

1 posit

ions

pla

tform

, an

d ca

lcul

ates

plo

ts.

GD

C-1

2 1

IU/A

ZIM

UT

H L

AY

ING

PR

OG

RA

M;

Alig

ns t

he p

latfo

rm to

the

firin

g az

imut

h.

IBM

I

GD

C-3

3 A

TT

ITU

DE

RA

TE

CO

MM

AN

D T

ES

T;

Exe

rcis

es t

he a

ttitu

de r

ate

chan

nels

afte

r IB

M

I switch

ing

to th

e S

-IB

bur

n m

ode.

GD

C-2

5 E

DS

TE

ST;

S

imul

ates

and

eva

luat

es t

he v

ehic

le a

nd s

pace

craf

t'usi

rj M

DO

s to

det

ect.

IBM

1

GD

C-2

2 L

SE

ELE

CT

RO

ME

CH

AN

ICA

L S

YS

TE

MS

TE

ST;

Ver

ifies

pro

per o

pera

tion

and

BA

TC

is

olat

ion

of r

edun

dant

LS

E re

trac

tion

syst

em,

incl

udin

g S

A,

TS

M a

nd H

DA

.

GD

C-3

3 F

LIG

HT

CO

NTR

OL

UT

ILIT

Y P

RO

GR

AM

S;

Dur

ing

maj

or te

sts,

it

sel

ectiv

ely

perfo

rms

IBM

I S-

IB e

ngin

e nu

ll te

st,

S-I

VB

eng

ine

null

test

, S

-IV

B c

oast

nul

l tes

t,

S-I

B n

ot z

ero

I lx1

1 I t

est,

and

spac

ecra

ft co

ntro

l che

cks

*MS

FC

Del

lver

ed P

rogr

am

20

6

thru

2

09

X X X X X X X X

X X X X X X X

XX

X

X

X X X

Link

ed b

y IA

LK,

LAG

C,

LAP

G

Link

ed b

y IA

LL

Link

ed b

y IA

TS

Sub

Pro

gram

s 12

33,

IZE

A,

IZR

E,

IZS

A,

IZM

L,

IZE

C

Link

ed b

y IA

LL

,LA

Fl

Sub

Pro

gram

s O

ZF

1,

LZ

F2

\J

Page 16: JOHN F. KENNEDY SPACE CENTER

Tabl

e 1-1

. S

atur

n IB

Ope

ratin

g S

yste

m a

nd T

est

Pro

gram

s (C

ontin

ued)

lVA

R

L/V

Sw

itch

Sel

ecto

r by

sta

ge.

GD

C-4

LI

NK

ING

PR

OG

RA

M F

OR

CO

UN

TDO

WN

; Li

nks

all p

rogr

ams

from

T-8

3 h

rs.

to

BA

TC

T

-75

hrs

,in

CD

DT

/CD

.

GD

C4

LI

NK

ING

PR

OG

RA

M F

OR

CO

UN

TDO

WN

; Li

nks

all

prog

ram

s an

d pe

rform

s pr

oced

ured

B

ATC

fu

nctio

ns f

rom

T-9

hrs

. to

T-1

hr.

51

min

. fo

r C

DD

T/C

D

GD

C4

LI

NK

ING

PR

OG

RA

M F

OR

OV

ER

ALL

TE

STS

; Li

nks

all p

rogr

ams

and

perfo

rtns

BA

TC

pr

oced

ural

func

tions

for

pro

pose

d tim

e pe

riod

of T

-1 h

r. 5

1 m

in.

to T

-3 5

min

. S

ub p

rogr

am:

LZ

TU

IN

S-2

1 R

AC

S R

AP

ID C

ON

TRO

L B

AC

KU

P;

Issu

es R

AC

S c

omm

ands

, as

req

uire

d,

for

HI,

LO,

or

BA

TC

R

UN

to a

ny s

tage

, or

all

stag

es.

tole

ranc

e vo

ltage

s w

ith a

ppro

pria

te e

rror

mes

sage

s.

Oth

er N

AS

A A

uth.

E

lem

: M

EC

-11

NA

SA

A

U~

.

EL

EM

EN

TA

ND

R

ES

PO

NS

IBLE

C

ON

TR

AC

TO

R

PRO

GR

AM

TIT

LE

4 F

UN

CTI

ON

INT

ER

FA

CE

ST

AT

US

AN

D/O

R

RE

MA

RK

S

AU

TM

. F

OR

NO

.

? - o 5

K

"3

Eg

+

g S$

w

;z:za,,,

~o

ur

~o

oO

ii

-*

:'.

w

Page 17: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

I6 O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

LAO

1

LAC

bl

LA

D0

LA

EM

sTA

rur

AN

O/O

R

Rru

Anr

s

Sub

pro

gram

s O

ZIT

, E

ZIT

, L

ZIT

, IZ

DS

, an

d lZ

Fl

Link

ed b

y IA

LL

, IA

LJ

Oth

er N

AS

A A

utb.

E

lem

: G

DC

-3.

Link

ed b

y [A

LL

pro

- gr

ams

IZT

T,

IZT

M,

IZG

T

Link

ed b

y L

AL

L

AU

TH

. F

OR

NO

.

20

6

t hru

MA

%

AU

TM

. E

LE

ME

NT

AN

0

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-2

2 B

AT

C

GD

C-2

B

AT

C

INS

-12

6 A

TC

GD

C-4

B

AT

C

GD

C-2

5 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-2

5 IB

M

42

6 (REV. 5

/69)

209

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

SW

ING

AR

M S

YS

TE

M P

OW

ER

UP;

S

can

all

S/A

sw

itche

s an

d in

dica

tors

dur

ing

pow

er

up t

o a

ssur

e co

mm

on i

nit

ial b

asel

ine.

L/V

SW

ITC

H S

ELE

CT

OR

IN

TE

RF

AC

E T

ES

T;

Pro

vide

s an

int

erfa

ce c

heck

of

the

L/V

S

WIT

CH

SE

LEC

TO

R B

Y S

TA

GE

.

L/V

TE

LE

ME

TR

Y C

ALI

BR

AT

ION

; P

rovi

des

auto

mat

ic c

alib

ratio

n se

quen

ce.

TE

RM

INA

L S

EQ

UE

NC

E P

RO

GR

AM

; P

rovi

des

linki

ng o

f a

ll th

e pr

ogra

ms

ri~

~i,

an

d au

tom

atic

ally

per

form

s pr

oced

ural

fun

ctio

ns d

urin

g te

rmin

al c

ou

~it

do

w~

~

sequ

eric

r.

Pro

pose

d tim

e pe

riod

T-1

5 m

in to

T-0

.

IU/P

OW

ER

U

P;

IU G

roun

d an

d S

tage

Pow

er a

pplic

atio

n;

auto

mat

es t

he m

anua

l co

mm

ands

to

app

ly g

roun

d po

wer

, st

age

pow

er,

and

IU te

mpe

ratu

re c

ontr

ol.

LVD

C C

OM

MA

ND

SY

ST

EM

TE

ST

; P

ower

s up

flig

ht c

ompu

ter,

and

runs

Pro

gram

s F

T3

4,

FT

08

, F

T3

5,

FT

20

, F

T2

3,

FT

45

, an

d F

T4

7.

LVD

C/D

A

DIS

CR

ET

E I

NP

UT

/3U

TP

UT

TE

ST;

Run

s F

T2

5 a

nd F

T9

3 a

nd t

ests

the

LV

DC

dis

cret

e in

put

and

outp

ut r

egis

ters

.

MIS

SIO

N E

VE

NT

S;

Pro

vide

s au

tom

atio

n of

the

SV

ele

ct m

ate

on l

inki

ng p

rogr

ams

FT

25

FT

33

, an

d fT

45

mar

king

test

s as

req

uire

d of

dis

cret

es a

nd a

llow

ing

dela

ys

for

spec

ial

S. C

. sw

itche

s to

be

oper

ated

. V

C4

X X X

X XX

d =: W X X

X

X

? - 0

0

-J X

m

ZO

O"

X X X

X

X

XX

,

XX

X

" xx

i X

XX

Y

X X

X K Y

INT

ER

FA

CE

0 g m

u

44

U>

Dg

$g

W

*O

U?

?~

00

0

X

X

X

X

Page 18: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IR O

pera

ting

Sys

tem

and

Tes

t P

rog-

-!ns (Cc..?!;;..,

I i lV

AR

LA

F2

LA

FC

LAG

C

LAG

1

LA

LL

LA

M1

LAP

G

LA

PW

KSC

rO

RM

-

- IN

TE

RF

AC

E

NA

SA

AU

TV

A

U rn

. E

LE

ME

NT

Ah

J

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-3

3 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

3 IB

M

GO

C-3

2 IB

M

ME

C-2

5

IBM

GD

C-3

2 IB

M

GD

C-3

2 IB

M

16-2

26 (

RE

V.

5/49

)

FO

R

, PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

ST

AT

US

AN

D.O

R

RE

MA

RK

S

Y~H

ICLe

0

-I

ur

NO

.

FL

IGH

T C

ON

TR

OL

PR

EP

S;

Pow

ers

up th

e F

light

Con

trol

Com

pute

r (F

CC

) an

d/or

th

e 2

06

E

DS

Con

trol

Rat

e G

yros

(C

RG

).

Fun

ctic

nally

che

cks:

FC

C m

ode-

switc

hing

and

com

- 1 t

iiru

para

tor

set;

FC

C a

nd C

RG

ram

ps a

nd p

ower

cir

cuits

; an

d th

e C

RG

am

p1 it

ude

and

20

9

com

para

tor

circ

uitr

y .

LVD

C/L

VD

A

FLI

GH

T C

ON

TR

OL

SY

ST

EM

IN

TE

RF

AC

E;

Clie

cl:~

for

prop

er o

pera

tion

betw

een

the

LV

DA

and

the

Flig

ht C

ontr

ol S

yste

m.

LVD

C/L

VD

A G

U!D

AN

CE

& C

ON

TR

OL

SlM

ULA

TE

D F

LIG

HT

SE

QU

EN

CE

L'E

R I

FI-

C

ATI

ON

; V

erifi

es G

&C

flig

ht s

wit

ch s

elec

tor

sequ

ence

and

ver

ifies

CIF

TM

dat

a re

duct

ion.

FLI

GH

T C

ON

TR

OL

GE

NE

RA

L IN

VE

ST

IGA

TIO

N;

Pro

vide

s ca

pabi

lity

of i

ssui

ny a

nd

obse

rvin

g FC

C F

UN

CT

ION

S a

nd m

easu

rem

ents

for

Tro

uble

sl~o

otin

y.

FLI

GH

T C

OM

PU

TE

R R

EP

ER

TO

IRE

PR

OG

RA

M;

Sel

ects

any

lig

ht c

om

pu

t~r A

TO

LL

pr

oced

ure

(LA

PW

, LA

CM

, LA

SS

, LA

GC

, LA

PG

, L

AS

T,

LA

RT

, L

AF

C).

GA

S B

EA

RIN

G S

UP

PLY

SY

ST

EM

OP

ER

ATI

ON

; P

ress

uriz

es t

he g

as b

earin

g sp

here

fo

r op

erat

ing

the

ST

12

4.

Ven

ts t

he s

pher

e 1

5 m

inut

es a

fter

tlre

ST

12

4 i

s po

wer

ed

I I X

dow

n.

LVD

C P

RO

GR

AM

LO

AD

; Lo

ads

pref

light

and

fliq

ht p

rogr

ams

intb

t!

~

LVD

C,

auto

- m

atic

ally

sel

ectin

g th

e be

st l

oadi

ng s

eque

nce

by c

all

Pro

gram

s F

T0

4,

FT

d5

, F

T0

7,

FT

23

, F

T3

7,

or F

T5

5.

LVD

C/L

VD

A

PO

WE

R O

N T

ES

T;

Mak

es a

flig

ht c

ontr

ol c

onfiq

urat

ion

arid

dis

cret

e st

atus

che

cks;

(P

rogr

ams

FT

04

, F

T0

8,

FT

35

, F

T2

0,

FT

23

wil

l be

lin

ked)

.

X

'4

1

XX

X

Page 19: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

A 1

1 NA

SA

AU

TH

. I

EL

EM

EN

TA

ND

CO

NT

RA

CT

OR

P

RO

GR

AM

TIT

LE

6 F

UN

CTI

ON

LA

RT

G

DC

-32

LVD

C/L

VD

A R

ED

UN

DA

NC

Y &

TM

R O

UTP

UT

DR

IVE

R T

ES

T;

Sel

ects

app

ropr

iate

IB

M

FT

B4

opt

ions

for

a g

iven

LV

DA

, i.e

.,

LV

DA

SN

P12 o

r lo

wer

, "T

MR

cha

nnel

sw

itchi

ng o

nly"

-S

N P

I 3 a

nd a

bove

, "f

ull

red

unda

ncy

chec

ks. "

I

GD

C-3

2 LV

DC

/LV

DA

CIU

& S

WIT

CH

SE

LEC

TO

R T

ES

T;

Pro

vide

s th

e ca

pabi

lity

to p

ower

up

( I I

BM

I and

pow

er d

own

the

flig

ht

com

pute

r, an

d p

erf

om

Pro

gram

s F

T0

3 a

nd F

T4

3.

GD

C-3

2 LV

DC

/LV

DA

- S

T1

24

INT

ER

FA

CE

TE

ST;

C

heck

s fo

r pr

oper

ope

ratio

n be

twee

n

I I IB

M

/ LVDA

and

the

ST

12

4 p

latfo

rm.

I LA5

W

I GFi2

5 I IU S

WIT

CH

SE

LEC

TO

R T

ES

T;

Che

cks

end

poin

t of

all

1U

switc

h se

lect

or c

hann

els

for

both

true

and

com

plem

ent

stat

e.

('M

E0

1

I INS-2

1

I RACS

RA

PID

CO

NTR

OL;

P

rovi

der

imm

edia

te c

ontr

ol o

f R

AC

S v

ia D

ispl

ay C

onso

le.

Ill

I*MTO

~ I IN

S-2

1

I MEA

SU

RE

ME

NT

CA

LIB

RA

TIO

N T

ES

T;

Ena

bles

the

test

eng

inee

r to

dir

ect

the

calib

ratio

n o

f the

RA

CS

Mea

sure

men

t S

yste

m.

I lXI

GD

C-3

3 S

-IS

HY

DR

AU

LIC

AC

TU

AT

OR

CA

LIB

RA

TIO

N;

Gen

erat

es a

n ac

tuat

or c

alib

ratio

n ta

ble

I OAAC

1 C

CC

D

1 to be u

sed

by p

rogr

ams

whi

ch re

quir

e ac

tuat

or p

ositi

on In

form

atio

n.

ME

C-2

3

S-IB

E

NG

INE

PU

RG

ES

; In

itiat

es e

ngin

e pu

rges

and

ver

ifies

pur

ges

are

actu

ated

wit

hin

I OAEP

/ CC

SD

1 a spe

cifie

d tim

e lim

it.

S-If

3 H

YD

RA

ULI

C S

YS

TE

M G

EN

ER

AL

SU

PP

OR

T; T

urns

on

mon

itors

aod

shu

ts d

own

any

com

bina

tion (1

thro

ugh

4) o

f the

hyd

raul

ic s

yste

ms

(use

d to

sup

pan

othe

r te

sts)

. \

OA

HF

I GD

C-3

3 S

-IB

AC

TU

AT

OR

/HY

DR

AU

LIC

S

YS

TE

M F

UN

CT

ION

AL

TES

T;

Per

form

s a

func

tiona

l X

X C

CS

D

chec

k of

all

four

hyd

raul

ic s

yste

ms.

C

ycle

s ac

tuat

ors

by c

alli

ng

LA

G1

and

read

s de

lta

I nu

ll le

vels

at

ambi

ent a

nd a

t 1

40

°F.

OA

HS

G

DC

-33

S-I

B H

YD

RA

ULI

C S

YS

TE

M R

EV

ER

IFIC

AT

ION

SU

PP

OR

T; T

urns

on,

m

onito

rs a

nd

X

X

CC

SD

sh

uts

dow

n an

y of

;he

four

hyd

raul

ic s

yste

ms.

C

onta

ins

optio

ns t

o c

alcu

late

flu

id

leve

l and

or

safe

the

sys

tem

aut

omat

ical

ly i

f ou

t of t

oler

ance

con

ditio

ns o

ccur

.

1 h

c FO

RM

16-

226

(RE

V.

56

9) I

11

1

*M S

FC

Del

iver

ed P

rogr

am

Page 20: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1.

Sat

urn

IB O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

1

AU

TH

. F

OR

v

~~

lC

L~

N

O.

OA

LB

ME

C-2

3

LOX

BU

BB

LIN

G A

ND

PR

ES

SU

RIZ

AT

ION

; P

erfo

rms

a fu

nctio

nal

test

of

the

LOX

C

CS

D

bubb

ling

syst

em.

Che

cks

inle

t te

mpe

ratu

re to

tole

ranc

e.

Bub

bles

the

sys

tem

and

ve

rifie

s pr

oper

tem

pera

ture

dec

reas

e an

d ch

ecks

pre

ssu

riz~

tio

n cy

cle

to b

e w

ith

in

its

time

limit

.

0AI.S

G

DC

-24

S-I

B L

OX

CA

VIT

Y S

EA

L T

EM

PE

RA

TU

RE

TE

ST

; V

erifi

es v

otin

g lo

gic

of L

OX

cav

ity

CC

SD

se

al t

empe

ratu

re s

enso

rs f

or e

ach

engi

ne b

y sw

ingi

ng R

AC

S t

o h

igh,

lo

w,

and

run

mod

es,

to s

imul

ate

high

and

low

tem

pera

ture

s.

driv

en i

ndic

ator

lam

ps,

switc

h-dr

iven

LD

I, a

nd a

ssoc

iate

d ca

blin

g.

OA

R1

GD

C-2

4 S

-IB

N

ETW

OR

KS

VE

RIF

ICA

TIO

N T

ES

T;

Ver

ifies

S-I

B s

tage

and

ES

E c

ircu

its

to

CC

SD

in

clud

e a

ll st

age

C/O

mod

es,

prev

alve

tim

ing,

po

wer

tran

sfer

, fl

igh

t se

quen

ce,

and

stag

e an

d E

SE

redu

ndan

t cir

cuits

.

delta

pre

ssur

es a

nd t

ests

for

in

tole

ranc

e pr

essu

res.

CC

SC

ov

eral

l tes

ts.

ST

AT

US

AN

Dx'

OR

RE

MA

RK

S

lVA

R

INT

ER

FA

CE

N

AS

A A

UT

H.

EL

EM

EN

T A

ND

R

ES

PO

NS

IBL

E

CO

NT

RA

CT

OR

PR

OG

RAM

TIT

LE

6 F

UN

CTI

ON

d 2

*

*:

2

w

K

0:

Z&

+

g w

;:

::

22

DL

zz

~

PU

%?

9P

OO

9 o 3

",

Page 21: JOHN F. KENNEDY SPACE CENTER

0

XX

XX

XX

XX

XX

X

x

W

X X

X

XX

X

XX

X

X

XX

XX

XX

XX

X

X

pa

l uo!leJlsuotuag um

opwno3

umopvno3 p

un

el

Page 22: JOHN F. KENNEDY SPACE CENTER

Table 1-2. Saturn I6 Major Test Program Matrix (Continued)

*AS-206 ONLY.

Page 23: JOHN F. KENNEDY SPACE CENTER

Table 1-2. Saturn IB Major Test Program Matrix (Continued)

*AS-206 ONLY.

Page 24: JOHN F. KENNEDY SPACE CENTER

--

.-

- --

x

x

x

x

Red

unda

ncy

Tes

t .-~

-

- . ..

-

x

x

x

x

x

x

S/V

O

AT

No.

1

-

--

(Plu

gs I

n)

X

X

X

S/V

E

lect

rica

l H

ate

--

X X

X

X

X

X

X

X

XX

--

.-

_ .

.

. .-

..

..

.

_

-

_-- -

x

x

x

x

x

x

x

x

x

x

-

.

. -

X

X

X

X

X

--

~

~-

- .. - .

--

-

-- -

-

I - -

- - . -. - -.

X X

X

X

X

X

X

X

X X

LV

S/A

O

AT

Laun

ch C

ount

dow

n

Cou

ntdo

wn

Dem

onst

ratio

n T

eL

S

/C

Bac

k U

p G

uida

nce

Tes

t

X X

X

X

X

X

F

ligh

t R

eadi

ness

T

est

x

x

x

ILV

G&C

Che

cks

LV

Ele

ctri

cal

x

x

x

x

x

x

x

X

-

~

--

X

X

X

-

--

XX

XX

X

X

X

XX

XX

XX

XX

X

XX

X

Mal

func

tion

OA

T -

-.

Sys

tem

s T

est

LV

Sta

ge o

r S

ub-S

yste

m

LV

Pro

pella

nt L

oad

All

Sys

tem

s T

est *

Page 25: JOHN F. KENNEDY SPACE CENTER

X

X

X X

X

X

X

~

X

X

--

XX

XX

X

X

X

X

X

X X

Laun

c:~ C

ount

dow

n --

Cou

ntdo

wn

Dem

onst

ratio

n Te

st

S/C

B

ack

Up

Gui

danc

e Te

st

-

Fi i

gM

Rea

dine

ss

Test

L

V F

light

Sys

tem

s R

edun

danc

y ~

es

t

SA

f O

AT

No.

1

(Plu

cts

In)

S/V

Ele

ctri

cal

Mat

e

LV

S/A

O

AT

~a

lfu

nc

ti~

n

OA

T

LV

G&

C C

heck

s L

V E

lect

rica

l Sy

stem

s Te

st

LV

Sta

ge o

r Su

b-Sv

stem

L

V P

rope

llant

Loa

d A

ll Sy

stem

s Te

st *

Page 26: JOHN F. KENNEDY SPACE CENTER

Tab

le 1-3.

Oth

er S

atur

n I6

Sys

tem

s P

rogr

ams

PRO

CR

AM

TIT

LE

h F

UN

CTI

ON

'"A

R

*AT

GT

C

AP

-A

AT

OL

L T

AP

E G

EN

ER

ATO

R (

AT

OL

L U

TIL

ITY

);

Pro

vide

s th

e ca

pabi

lity

to u

pdat

e th

e / IB

M

/ ATOL

L d

rum

ind

ex.

NA

SA

AU

TH

. E

LE

UE

WT

AN

D

RE

SrO

NS

l8L

E

CW

TR

AC

TO

R

DD

TC

C

AP

-A

DIS

PLA

Y D

ES

CR

IPT

ION

TA

PE

GE

NE

RA

TOR

; G

ener

ates

the

DD

tap

e fro

m

/ IBM

I sym

bolic

inp

ut.

DE

04

G

DC

-31

M

LC

INS

TR

UC

TIO

N T

ES

T,

PA

RT

1; V

erifi

es t

hat

all

but

tlte

I/O

and

som

e co

ntro

l op

( IBu

1 code

s pedm

pro

perly

.

DE

05

G

DC

-31

MLC

DR

UM

TE

ST

; V

erifi

es,

in le

ss th

an c

ert

ai:~

test

, th

at d

ata

can

be t

rans

ferr

ed t

o I IB

M

md

hm

the

dru

m.

DE

06

G

DC

-31

ML

C M

EM

OR

Y T

ES

T;

Per

form

s a

curs

ory

chec

k of

HS

M fo

r th

e LC

C.

I IBM

I

DE

07

G

DC

-31

ML

C IN

ST

RU

CT

ION

TE

ST

, P

AR

T 2

; V

erifi

es t

hat

all

but t

he I

/O a

nd s

ome

cont

rol o

p I IB

M

1 codes

per

form

pro

perly

for

the LCC.

DT

02

IN

S-1

3

SG

CC

DD

AS

CU

RS

OR

Y T

ES

T;

Pro

vide

s a

curs

ory

test

of

the

DD

AS

IOD

C a

rd c

ompu

ter

/ IB.

I inteda

ce u

nit.

DT

Ol

DT

12

G

DC

-31

R

U-1

10

A/D

DP

-22

4

INT

ER

FA

CE

CH

EC

KO

UT;

P

erfo

nns

an o

n-lin

e ch

ecko

ut o

f th

e 1 IB

M

I RU-1

lOA

IO

DC

-6 a

nd t

he D

DP

-22

4 f

ully

buf

fere

d ch

anne

l and

indi

cate

s m

alfu

nctio

n. I

GD

C-3

1 S

GC

C G

MT

MA

INT

EN

AN

CE

TE

ST;

E

xerc

ises

the

oper

atio

n of

the

GM

T cl

ock,

w

hile

IB

M

/ running

und

er th

e co

ntm

l of

the

Sat

urn

oper

atin

g sy

stem

.

FA

CE

7 Y x x x x x

DT

13

G

DC

-31

LCC

INS

TR

UC

TIO

N T

ES

T;

Ver

ifies

tha

t a

ll bu

t th

e 1/

0 an

d so

me

cont

rol o

p co

des

Isu

1 perform

prop

erly

.

*MS

FC

D

eliv

ered

Pro

gram

ST

AT

US

AN

D/O

R

RE

MA

RK

S

Inte

rrel

ated

w/D

T1

3

[&er

rela

ted

w/D

T1

4

4

2

0 " 0 X X X

DT

14

DT

15

AUTn

. F

OR

V

EH

ICL

E

NO

. l- I

U

X

m FO

RM

IC

iH (

RE

V.

5/6

9)

GD

C-3

1 I

LCC

DR

UM

TE

ST

; V

erifi

es,

in le

ss t

han

cert

ain

test

, th

at d

ata

can

be t

rans

ferr

ed t

o IB

M

GD

C-3

1 IB

M

i an

d fro

m th

e dr

um.

LC

C M

EM

OR

Y T

ES

T;

Per

form

s a

curs

ory

chec

k of

IS

M.

I X

X

Page 27: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-3.

Oth

er S

atur

n IB

Svs

tem

s P

roar

ams

(Con

tinue

d)

ST

AT

US

AN

D/O

R

RE

MA

RK

S

C-l

I h~

0

Inte

rrel

ated

Wh

T0

2

Link

ed b

y IA

LL

WS

FC

Del

iver

ed P

rogr

am

lV

a

DT

P2

DT

SC

DT

23

EN

RS

WU

O 1

WT

94

WT

97

WT

98

*T9

9/

NE

99

WT

DR

i

I

Y 6-3

( E

V.

5,69

1

MA;

* *u

rn.

ELE

ME

NT

Am

, R

E$

W~

I.L

E

CO

NT

RA

CT

OR

INS

-13

IBM

GD

C-3

1 IB

M

GD

C-3

1 IS

M

GD

C-3

1 C

AP

-B

GD

C-3

2 IB

M

CA

P-A

IB

M

CA

P4

IB

M

CA

P4

IB

M

CA

P4

IS

M

CA

P*

IBM

~.

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

DD

AS

CU

RS

OR

Y T

ES

T.

LCC

SE

LF-C

HE

CK

; M

onito

rs th

e pe

riphe

ral e

quip

men

t with

in th

e LC

C to

det

erm

ine

its

oper

atio

nal s

tatu

s.

LCC

ON

-LIN

E P

ER

IPH

ER

AL

EQ

UIP

ME

NT

TE

ST;

P

rinte

r, ta

pe s

tatio

ns 1

-3,

& 2

-9

card

read

er.

MLC

SLO

W S

YS

TE

M R

EC

OV

ER

Y B

OO

T S

TRA

P;

Load

s M

LC U

XE

X L

oade

r/M

odifi

er

from

MLC

MT

S 1

-3 o

r 2

-3 (

desi

gned

for

rem

ote,

au

tom

atic

slo

w s

yste

m re

cove

ry).

SIM

ULA

TE

D P

LUS

-TIM

E T

AB

LE G

EN

ER

ATO

R T

ES

T; 3

uns

valid

ity c

heck

s on

a

sim

ulat

ed p

lus4

ime

card

dec

k fo

r ei

ther

tow

er t

est,

stat

ion

acqu

isiti

on,

or c

omm

and

func

tions

; m

ite

s de

ck.

DC

C R

EM

OTE

LO

AD

NN

LOA

D;

Dis

play

con

trol

com

pute

r lo

ad/u

nloa

d pr

ogra

m re

spon

ds

to d

iscr

etes

ini

tiate

d fro

m d

iscr

ete

pane

l, an

d ei

ther

rei

oads

the

DC

C o

r du

mps

the

DC

C

on p

rinte

r or

log

tape

. I

DIS

CR

ET

E A

CT

IVIT

Y M

ON

ITO

R T

ES

T; P

rovi

des

the

stat

us a

nd n

umbe

r of

LD

ls a

nd

MD

ls n

ot i

n a

pre

spec

ified

sta

te f

or o

ne o

r a

ll st

ages

.

LV

DIS

CR

ET

E IN

ITIA

LIZ

AT

ION

; D

ispl

ays

and

prin

ts th

e st

atus

of

all

MD

ls a

nd L

Dls

.

DIS

CR

ET

E E

XE

C.

TA

BLE

MO

DIF

Y;

Pro

vide

s th

e ca

pabi

lity

to m

odify

, on

line

, th

e D

iscr

ete

Act

ion

Tab

le.

LA/

DIS

CR

ET

E R

ES

PO

NS

E T

IME

; M

easw

es th

e el

apse

d tim

e be

twee

n th

e is

suan

ce o

f M

DO

and

MD

I, or

, D

DA

S d

isae

te t

alkb

ack.

11

0, - o

0 n

a\

u iY i I

INT

ER

FA

CE

xE

5

XX

XX

a

X

XX

X

X

X

X

X

XX

X

0-

I

z2

O

b

:~

l:

zg

a;

=

I

/X

=>

a,

X

'X

X

X

X

X

I

c3 X

X

X

Page 28: JOHN F. KENNEDY SPACE CENTER

--

IVA

R

Tab

le 1

-3.

Otl

~e

r Sat

urn

I6 S

yste

n~s P

royr

arns

(C

ontin

gedl

INT

ER

CA

C

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

AE

SP

ON

SIB

LE 1

PRO

GR

AM

TIT

LE

h F

UN

CTI

ON

C

ON

TR

AC

TO

R

ALT

ER

NA

TE

ME

MO

RY

CH

EC

KE

R;

Fun

ctio

n ex

ecut

or u

sed

to c

heck

out

redu

ndan

t 1%

M

I mem

ory

of M

L c

ompu

ter.

(160

-4

IBM

A

NA

LOG

TE

ST

PO

INT

MO

NIT

OR

; M

cnito

rs a

spe

clfl

c ha

rdw

lre a

nalo

g te

st

poin

t, an

d di

spla

ys e

ach

valu

e re

ad (

keyb

oard

ent

ry m

ust

be m

ade

for

each

tes

t pe

lnt

to b

e m

onito

red)

. U

pdat

es f

or b

ias,

si

gnal

ran

ge,

and

cles

crlp

tion

lnay

be

ente

red.

S

E8

8 m

ay a

lso

be ~

~s

ed

to

del

ete-

an a

ctiv

e an

alog

clo

t fro

m t

he m

onito

r ta

ble.

C

ontr

ol o

f the

rou

tine

is v

la th

e dl

spla

y co

nsol

e ke

yboa

rd.

CA

P-A

IB

M

CA

P-A

R

EC

OV

ER

Y D

UM

P R

ET

RIE

VA

L; P

rovi

des

the

capa

bilit

y to

log

tlie

ML

C b

inar

y du

mp

IBM

I on l

og ta

pe,

and

pres

ent

reco

very

and

the

sys

tem

sta

tus.

DIS

CR

ET

E M

AS

K/U

NM

AS

K

RO

UTI

NE

; M

odifi

es,

by m

aski

ng o

r un

mas

king

, th

e in

terr

upt

corlt

rol

wor

d gr

oups

. It

acc

epts

dat

a w

liich

wil

l mod

ify th

e LC

CC

or

ML

C

disc

rete

mon

itor

inte

rrup

t (M

I) c

ontr

ol w

ords

. If

a g

roup

is

mas

ked,

any

clia

~ig

e ill

Dl

CA

P-A

IS

M

RE

MO

TE

LO

AD

PR

ELO

AD

- LO

AD

BO

OT

ST

RA

P

ISM

C

AP-A

I st

atus

car

lnot

cau

se a

n in

terr

upt.

If th

e gr

oup

is u

nmas

ked,

an

inte

rrup

t ca

r1 b

e al

low

ed

whe

n a

Dl

chan

ge i

s de

tect

ed.

AI!

dis

cret

egro

ups

may

!)e u

rimas

kedw

ith J

ne k

eyb

~a

rd

I ent

ry.

ML

C R

EC

OV

ER

Y C

ON

TRO

L;

Thi

s pr

oqra

nl i

s th

e co

ntro

lliny

pro

gram

for

ML

C S

yste

m

Rec

over

y (S

SR

P)

Opt

ions

, by

allo

win

g ei

ther

sta

rtin

g of

the

rec

over

y pr

oces

s or

ter

tnin

a-

tion.

If

reco

very

is

star

ted,

th

e pr

ogra

m d

ispl

ays

tuto

rial

mes

sage

s to

sta

rt r

ccov

ery

at

the

ML

C.

The

LC

CC

is

set

to D

OW

N s

tatu

s, a

rid i

nter

rupt

s ar

e in

hibi

ted.

C

omm

unic

a-

tian

s w

ith

the

ML

C S

yste

m R

ecov

ery

are

then

beg

un.

GD

C-3

1 S

YS

TE

M C

LOS

EO

UT;

P

fovi

des

optio

ns t

o du

~lll)

IOR

-2s,

co

re,

and

drum

to

a lo

g ta

pe;

IBM

1 and/

or

clos

es o

ut t

hat.

log

tapc

.

C111,m

IBM

*MS

FC

D

eliv

ered

Pro

grdm

ML

C R

EM

OT

E L

OA

D;

Init

iall

y lo

ads

the

ML

C O

pera

ting

Sys

tem

fro

m t

l~e

LCC

C s

yste

m

Mas

ter

Tape

, to

allo

w p

atch

ing

of M

LC

cor

e an

d dr

um r

esid

en!

prog

ram

s, a

nd tc

l lo

ad

func

tion

exec

utor

bin

ary

card

dec

ks.

CA

P-B

O

N-L

INE

D

AT

A R

ET

RIE

VA

L (P

OS

TPR

OC

ES

SIN

G);

E

nabl

es a

qui

ck-lo

ok c

lisc.

rcte

I da

ta r

etri

eval

.

Page 29: JOHN F. KENNEDY SPACE CENTER

Tabl

e 1-4. S

atur

n V

Ope

ratin

g Sy

stem

and

Tes

t Pr

ogra

ms

PRO

GRA

M T

ITLE

6 F

UN

CTI

ON

"S..

. '"".

..,...s I"=

-. -

Is.,

* MS

FC D

eliv

ered

Pro

gram

Page 30: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

I5

C r

QR

M 1

0-2

16

(REV. 5

. 69

1

*MS

FC

Del

iver

ed P

rogr

am

AU

TM

. F

OR

V

En

lCL

~

NO

.

51

2/1

v'

lVA

R

*FT

04

*FT

05

xF

T0

6

* FT

07

*FT

08

*FT

10

*FT

20

* FT

23

* FT

25

* FT

27

* FT

31

- - - .

. -

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-3

2 IS

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IS

M

GD

C-3

2 IS

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

- - .

. - - . . . . - .

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

LVD

C/P

OW

ER

O

N-O

FF A

ND

/OR

R

ED

UN

DA

NC

Y T

ES

TS;

Pro

vide

s th

e ca

pabi

lity

of

appl

ying

or

rem

ovin

g po

wer

to

the

LVD

C/L

VD

A,

and/

or

perfo

rms

chec

king

func

tions

.

LVD

C/D

ATA

LO

AD

AN

D/O

R V

ER

IFY

TE

ST;

P

rovi

des

the

capa

bilit

y of

loa

ding

dat

a in

to,

and/

or

veri

fyin

g da

ta w

ithin

, th

e LV

DC

mem

ory

from

a g

iven

poi

nt.

LVD

C/G

IMB

AL

AN

GLE

RE

AD

TE

ST;

O

utpu

ts th

e gi

mba

l an

gle

stat

us,

utili

zing

the

Gim

bal A

ngle

Mon

itor

Pro

gram

in

the

LVD

C.

LVD

C/S

E L

EC

TOR

DU

MP

TE

ST

; C

omm

ands

the

prin

tout

of

LVD

C m

emor

y se

ctor

.

LVD

C C

OR

E M

AP

LO

AD

AN

D/O

R

PR

INT

TES

T;

Ret

rieve

s th

e C

ore

Map

fror

n th

e LV

DC

, st

ores

it

in th

e A

GC

SC

or

MLC

, an

d pr

ints

it

on th

e LC

C li

ne p

rint

er.

LVD

C/L

VD

A

LAD

DE

R O

UTP

UT

TES

T;

Exe

rcis

es t

he l

adde

rs to

pro

ve t

he L

VD

A's

st

eerin

g co

mm

and

capa

bilit

y .

LVD

C/L

VD

A

SE

LF-T

E S

T;

Per

form

s an

err

or c

heck

of

the

LVD

A/L

VD

C,

utili

zing

, w

here

pra

ctic

al,

the

LVD

C v

sutin

es t

o pe

rform

the

err

or c

heck

ing.

LVD

C/S

EC

TOR

SU

M C

HE

CK

; P

rovi

des

the

capa

bilit

y of

det

ernl

lnin

g if

any

spe

cifie

d LV

DC

mem

ory

sect

or h

as a

val

id c

heck

sum

.

LVD

C/L

VD

A

DIS

CR

ET

E I

NP

UT

TE

ST;

V

erifi

es th

at t

he L

VD

C c

an p

rope

rly r

ead

its

disc

rete

inpu

ts.

SIM

ULA

TE

D F

LIG

HT

MO

NIT

OR

TE

ST;

M

onito

rs a

nd r

ecor

ds th

e ev

ents

res

ultin

g fr

om t

he o

pera

tion

of t

he F

light

Sim

ulat

ion

Rou

tine

in th

e LV

DC

.

LVD

C A

CC

ELE

RO

ME

TE

R P

ULS

E C

OU

NT

TES

T;

Exe

rcis

es th

e A

ccel

erom

eter

P

ulse

Cou

nt R

outin

e of

the

LVD

C to

ens

ure

func

tioni

ng o

f th

e ac

cele

rom

eter

pro

cess

or

asso

ciat

ed w

ith th

e S

T-1

24

M p

latfo

rm a

ccel

erom

eter

s.

ST

AT

US

AN

D,

OR

RE

MA

RK

S

Link

ed b

y V

ALK

, K

PC

M,K

AG

l,KA

PG

, K

AP

W,

and

KA

RD

Link

ed b

y V

ALK

, K

AG

1, a

nd K

AP

G

Link

ed b

y V

4LK

, V

ALL

, V

AT

S,

and

VA

RY

Li

nked

by

KA

PG

Link

ed b

y V

ALK

, K

AC

M,

and

KA

PW

Link

ed b

y V

ALK

, V

ALL

, K

AC

M,

and

VA

RY

Li

nked

by

VA

LK,

WC

M, a

nd K

AP

W

Link

ed b

y V

ALK

, V

ALL

, K

AP

G,

and

KA

PW

Link

ed b

y K

AD

O,

KA

GI,

and

VA

LJ

Link

ed b

y V

AT

S

Link

ed b

y VA

L.

INT

ER

FA

CE

.

'? - u

0

-'

m X

0-

'

I lX i

0

;:

gz

zE

k+

z

z

<o

ue

Zo

oO

X'

+5

I

X X X X X X X

X X X X X X

KZ

X

X X X X

/ X X

X X

X X

Page 31: JOHN F. KENNEDY SPACE CENTER

Tr;

Jle

1-4

. S

atur

n V

Ope

ratin

g S

yste

m a

nd T

est

Pro

gram

s (C

ontin

ued)

NA

SA

AU

TH

. E

LEM

EN

T A

ND

IV

AR

1 RESP

ON

SIB

LE

I P

RO

GR

AM

TIT

LE

6 F

UN

CTI

ON

3

I 2 I LVD

C/L

VD

A D

ISC

RE

TE

OU

TPU

T TE

ST;

V

erifi

es t

hat

the

LVD

C d

iscr

ete

outp

uts

can

be s

et a

nd r

eset

.

LVD

C/L

VD

A

DD

AS

TE

ST;

V

erifi

es p

rope

r ope

ratio

n of

the

inte

rfac

e be

twee

n th

e LV

DC

tele

met

ry b

uffe

r and

the

DD

AS

.

*FT

37

G

DC

-32

SIM

ULA

TE

D F

LIG

HT

IN

ITIA

LIZ

E;

Pro

vide

s ha

rdw

are

chec

ks a

nd ic

idic

ator

wor

ds t

o IB

M

the

Sim

ulat

ed F

ligh

t M

onitc

r.

Com

man

ds L

VD

C to

the

follo

win

g m

odes

: a.

P

repa

ratio

n to

labn

ch w

ithou

t a

plat

form

. b.

P

repa

ratio

n to

laun

ch S

imul

ated

Flig

ht w

ith a

pla

tform

. c.

R

epea

tabl

e S

imul

ated

Flig

ht.

*FT

42

G

DC

-32

PR

EP

AR

E T

O L

AU

NC

H;

Pro

vide

s ha

rdw

are

chec

ks,

LVD

C i

nitia

lizat

ion,

an

d SG

CC

/ (B

M

1 initial

izat

ion

for

Flig

ht P

rogr

ams.

*FT

43

G

DC

-32

LVD

C C

OM

PU

TER

IN

TE

RF

AC

E U

NIT

TE

ST;

V

erifi

es C

IU o

pera

tion

with

in th

e X

IBM

In

stru

men

t Uni

t S

yste

m.

Tes

t O

pera

tion

of th

e G

uida

nce

Sys

tem

in

add

ress

ing

and

I re

ceiv

ing

data

from

the

CIU

.

*FT

45

G

DC

-32

LVD

C C

OM

MA

ND

SY

ST

EM

TE

ST;

V

erifi

es o

omm

unic

atio

n at

AG

CS

C b

etw

een

X 1 IB

M

Gui

danc

e C

omm

and

Sys

tsm

and

LV

DA

/LV

DC

. C

kc

ks

sig

nal

stre

ngth

in

Gui

danc

e C

omm

and

Rec

eive

r and

Dig

ital D

ecod

er.

1

PR

EF

LIG

HT

CO

MM

AN

D T

ES

T;

Com

man

ds th

e O

rbita

l Rou

tine

of t

he F

ligh

t P

rogr

am

ISM

*F

T4

7

I GDC

-32

I to e

nabl

e co

mm

unic

atio

n w

ith th

e LV

DC

.

"FT

49

G

DC

-32

AC

CE

LE

RO

MT

ER

MO

NIT

OR

DIS

PLA

Y C

ON

TRO

L;

Dis

play

s op

tions

for

and

IBM

ex

ecut

es F

E5

0.

*FT

54

G

DC

-32

LVD

C S

TEE

RIN

G T

ES

T;

Com

man

ds L

VD

C to

ent

er g

uida

nce

and

cont

rol

Ste

erin

g j I

BM

/ Tes

t and

to

retu

rn L

vD

c to

Moe

e so

n.

ill

55

1 Gqp

2 I LV

DC

TE

LEM

ET

RY

TE

ST

; C

omm

ands

the

LVD

C to

ent

er a

tele

met

ry t

est

rout

ine,

an

d lo

ads

an i

nput

wor

d to

spe

cify

the

rate

of

tele

met

ry.

I *M

SFC

D

eliv

ered

Pro

gram

Page 32: JOHN F. KENNEDY SPACE CENTER

KA

Ol

KA

CM

KA

DO

KA

Fl

FO

RM

*M

S F

C

Tab

le 1

-4.

Sat

urn

V O

pera

tiny

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

,')

--

- --

-

L--

ST

AT

US

AND

. OR

RE

MA

RK

S

Lin

ked

by

VA

LL

an

d V

AR

Y

Link

ed b

y V

AL

J

Link

ed b

y K

AL

L

Link

ed b

y V

AL

J

Link

ed b

y V

ALK

, V

AL

L,

KA

Fl

Link

ed b

y V

AT

S

AU

TM

. F

OR

V

~H

,C

L~

no

.

51

2,'

NA

SA

AU

~.

E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-3

2 IB

M

GD

C-1

2 IB

M

GD

C-1

2 IB

M

GD

C-2

5 IB

M

GD

C-3

2 IB

M

GD

C-3

2 IB

M

GD

C-3

3 IB

M

GD

C-3

3 IB

M

GD

C-3

3 IB

M

51

3

PR

OG

RA

M 1 IT

LE

6 F

UN

CT

ION

SIM

ULA

TE

D F

LIG

HT

PO

STP

RO

CE

SS

OR

TE

ST;

P

rovi

des

the

capa

bilit

y of

pr

oces

sing

the

raw

dat

a ge

nera

ted

by t

he o

vera

ll S

imul

ated

Flig

ht T

est

Pro

gram

.

AZ

IMU

TH

PO

SIT

ION

ING

AN

D M

ON

ITO

R P

G;

Mon

itors

the

azim

uth

enco

der

for

drift

, po

sitio

ns p

latfo

rm,

and

calc

ulat

es p

lot.

IU/A

ZIM

UT

H L

A'J

ING

P

RO

GR

AM

; A

ligns

the

pla

tform

to t

he f

irin

y az

imut

h.

IU/P

OW

ER

UP;

IU

Gro

und

and

Sta

ge P

ower

app

licat

ion;

aut

omat

es t

he t

nanu

al

com

man

ds t

o a

pply

gro

und

pow

er,

stag

e po

wer

, an

d IU

tem

pera

ture

con

trol

.

LVD

C C

OM

MA

ND

SY

ST

EM

TE

ST

; P

ower

s up

flig

ht c

ompu

ter,

and

rutis

Pro

gram

s F

T0

4,

FT

08

, F

T3

5,

FT

20

, F

T2

3,

FT

45

, an

d F

T4

7.

LVD

C/D

A

DIS

CR

ET

E I

NP

UT

/OU

TP

UT

T

ES

T;

Run

s F

T2

5 a

nd F

T3

3 a

nd t

ests

the

LV

DC

dis

cret

e in

put

and

outp

ut r

egis

ters

.

T-2

4 H

OU

RS

FL

IGH

T C

ON

TRO

L LI

NK

ING

; L

inks

all

Flig

ht

Con

trol

Pro

gram

s pe

rform

ed b

etw

een

T-2

4 a

nd T

-18

Hou

rs i

n th

e C

DD

T an

d C

D (

Pro

gram

s K

AF

2,

CT

C1,

C

TC

4,

CT

C5,

an

d V

AF

C).

FL

IGH

T C

ON

TRO

L P

RE

PS

; P

ower

s up

the

Flig

ht

Con

trol

Com

pute

r (F

CC

) an

d/or

the

E

DS

Con

trol

Rat

e G

yros

(C

RG

). F

unct

iona

lly c

heck

s:

FCC

mod

e-sw

itchi

ng a

nd

com

para

tor

set;

FCC

and

CR

G r

amps

and

pow

er c

ircu

its;

and

the

CR

G a

mpl

itude

and

co

mpa

rato

r cir

caitr

y.

FLI

GH

T C

ON

TRO

L F

LIG

HT

VE

CTO

R;

Aut

omat

ical

ly c

ompu

tes

the

S-IC

E

ngin

e T

hrus

t V

ecto

r to

sat

isfy

the

Lau

nch

Mis

sio

n R

ules

. R

edlin

e re

quire

men

t for

hol

ddow

n po

st

INT

ER

FA

CE

Y/

-2Y

(R

EV

. L

'69

) )e

l iver

ed

and

tow

er c

lear

ance

.

Pro

gram

X

Xx

X

X

- u

0

J br

v4

sm

XIXX

X

X X X

X

X

X

X

X

wu

,

=d

gz

za

gs

<

ou

99

oo

o

X

-, ~5

X X

X I

X I

X I X

I I

XiX

X X

X X X

X

X X

X

Page 33: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

PRO

GR

AM

TIT

LE

6 F

UN

CT

ION

t h) "

LVD

C/A

FLI

GH

T C

ON

TRO

L S

YS

TE

M I

NTE

RFA

CE

; C

heck

s fo

r pr

oper

ope

ratio

n be

twee

nthe

LV

DA

and

the

Flig

ht C

ontro

l S

yste

m.

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

FLI

GH

T C

OM

PU

TER

SY

ST

EM

CD

DT/

CD

SU

PP

OR

T P

RO

GR

AM

; Li

nks

Pro

gram

s F

T4

5,

FT

25

, F

T0

4,

and

FT

05

that

are

run

bet

wee

n T

-20

and

T-

18

Hou

rs.

KA

GC

FLI

GH

T C

OM

PU

TER

RE

PE

RTO

IRE

PR

OG

RA

M;

Sel

ects

any

flig

ht c

ompt

~ter

AT

01 L

pr

oced

ure

(KA

PW

, K

AC

M,

KA

SS

, K

AG

C,

KA

PG

, K

AS

T,

KA

RD

, K

AF

C).

MIS

SIO

N E

VE

NTS

; P

rovi

des

auto

mat

ion

of S

.V.

Ele

ct.

Mat

e by

lin

king

Pro

gram

s F

T2

5,

FT

33

, an

d F

T4

5,

mak

ing

test

s as

req

uire

d of

dis

cret

es a

nd a

llow

ing

dela

ys

for

spec

ific

S.C

. sw

itche

s to

be

oper

ated

.

GD

C-3

2 IB

M

LVD

C/L

VD

A G

UID

AN

CE

& C

ON

TRO

L S

IMU

LAT

ED

FLI

GH

T S

EQ

UE

NC

E V

ER

IFI-

C

ATI

ON

; V

erifi

es G

&C f

light

sw

itch

sele

ctor

seq

uenc

e an

d ve

rifie

s C

IF T

M d

ata

redu

ct io

n.

KA

M2

M

EC

-25

ME

CH

AN

ICA

L S

YS

TE

M F

UN

CTI

ON

AL;

Che

cks

that

IU

Pne

umat

ic C

onso

le a

nd

I 1 IB

M

1 Ther

mal

Con

ditio

ning

Sys

tem

is

oper

atin

g pr

oper

ly.

KA

Ml

LVD

C P

RO

GR

AM

LO

AD

: Lo

ads

pref

light

and

flig

ht p

rogr

ams

into

the

LVD

C,

auto

- m

atic

ally

sel

ectin

g th

e be

st l

oadi

ng s

eque

nce

by c

allin

g P

rogr

ams

FT

04

, F

T0

5,

FT

07

, F

T2

3,

FT

37

, or

FT

55

.

ME

C-2

5 IB

M

KA

PW

G

DC

-32

LVD

C/L

VD

A P

OW

ER

ON

TE

ST;

Mak

es a

7ig

ht c

o;ltr

ol c

onfig

ural

ion

and

disc

rete

I I IB

M

1 stat

us c

heck

s; (

Pro

gram

s F

T04

, F

T0

8,

FT

35

, F

T20

, F

T2

3 w

ill b

e lin

ked)

.

GA

S B

EA

RIN

G S

UP

PLY

SY

ST

EM

OP

ER

AT

ION

; P

ress

uriz

es t

he g

as b

earin

g sp

l~er

e fo

r op

erat

ing

the

ST

12

4.

Vent

s th

e sp

here

15

min

utes

afte

r th

e S

T1

24

is

pow

ered

do

wn.

KA

PS

G

DC

-12

lB FJ

l S

T1

24

PO

WE

R O

N S

EQ

UE

NC

ES

; P

ower

s on

the

ST

12

4 a

nd d

ispl

ays

all

ST

12

4

func

tions

and

mea

sure

men

ts d

urin

g po

wer

on

sequ

ence

s.

Page 34: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

AU

TN

. F

OR

y

EN

ICL

~

NO

.

51

2/

FT

04

opt

ions

for

a g

iven

LV

DA

, i.e

., LV

DA

SN

P1

2 o

r lo

wer

, "T

MR

cha

nnel

PR

OG

RA

M T

ITL

E &

FU

NC

TIO

N

LVD

C/L

VD

A

RE

DU

ND

AN

CY

& T

MR

OU

TP

UT

DR

IVE

R T

ES

T;

Sel

ects

app

ropr

iate

lVA

R

KA

RD

INT

ER

FA

CE

I

NA

SA

AU

TN

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-3

2 513

X

5%

I

-2

X

P 0" -I

X

X

Lin

kd

by

VA

LJ

-- --

X

XX

XX

--

0 2

2

2:

;

g~

~~

~g

;

<O

""

"O

OO

"l

X

I ST

AT

US

AN

D'O

R

RE

MA

RK

S

switc

hing

onl

y" -

SN

P1

3 a

nd a

bove

, "f

u!l

red

unda

ncy

chec

ks."

ST

12

4 P

LA

TF

OR

M S

ER

VO

LO

OP

DA

MP

ING

TE

ST

; T

ests

eac

h gy

ro a

nd a

ll se

rvo

loop

s.

LVD

C/L

VD

A C

IU &

SW

ITC

H S

EL

EC

T3

R T

ES

T:

Pro

vide

s th

e ca

pabi

lity

to p

ower

up

and

pow

er d

own

the

flig

ht c

ompu

ter,

arld

per

form

Pro

gram

s F

T0

3 a

nd F

T4

3.

LVD

C/L

VD

A -

ST

12

4 I

NT

ER

FA

CE

TE

S T;

C

heck

s fo

r pr

oper

ope

ratio

n be

twee

n L

VD

A a

nd t

he S

T1

24

pla

tform

.

KA

SD

I

KA

SS

KA

ST

d

X

IBM

GD

C-1

1 IB

M

GD

C-3

2 IS

M

GD

C-3

2 lB

fA

Link

ed b

y K

AL

L

KA

SW

xM

EO

l

*MT

Ol

QA

EC

QA

ES

QA

LS

GD

C-2

5 I I

U S

WIT

CH

SE

LEC

TO

R T

ES

T;

Che

cks

end

po

i~~

t of

all

IU s

wit

ch s

elec

tor

chan

nels

IB

M

INS

-21

INS

-21

GD

C-2

6 N

AR

ME

C-2

2

NA

R

GD

C-2

6 N

AR

for

both

true

and

cor

rple

men

t sta

te.

RA

CS

RA

PID

CO

NTR

OL;

Pro

vide

s im

med

iate

con

trol

of

RA

CS

via

Dis

play

Con

sole

.

ME

AS

UR

EM

EN

T C

ALI

BR

AT

ION

TE

ST

; E

nabl

es th

e te

st e

ngin

eer

to d

irec

t th

e ca

libra

tion

of t

he R

AC

S M

easu

rem

ent

Sys

tem

.

S-I

1 F

NG

INE

ELE

CT

RIC

AL

CIR

CU

ITR

Y T

ES

T;

Che

cks

engi

ne c

ontr

ol l

ogic

, ve

rifie

s en

gine

cut

off

CM

DS

; ch

ecks

out

eng

ine

spar

k sy

stem

, an

d pe

rfoi

ms

an e

ngin

e se

quen

ce

test

with

out

cont

rol p

ress

ures

.

S-l

l E

NG

INE

SE

QU

CN

CE

TE

ST

; A

fter

veri

fyin

g st

art

conf

igur

atio

n,

issu

es a

ll en

gine

st

art

com

man

ds a

nd th

en v

erifi

es t

hat

requ

ired

resp

onse

s oc

cur

wit

hin

spec

ified

lim

its

and

time

frw

s.

Issu

es e

ngin

e cu

toff

and

ver

ifies

app

ropr

iate

func

tions

for

shu

tdow

n se

quen

ce.

S-l

l P

RO

PE

LLA

NT

LE

VE

L &

DE

PLE

TIO

N S

EN

SO

RS

; V

erifi

es !h

at

the

leve

l, de

plet

ion,

fa

st-f

ill,

3nd

over

fill

sens

ors

(inc

ludi

ng l

ogic

and

tim

er c

ircu

itry)

ope

rate

pr

oper

1 y .

Page 35: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

IVA

R

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

P

RO

GR

AM

TIT

LE

6 F

UN

CT

ION

QA

MS

M

EC

-22

S

-ll

MA

INS

TA

GE

CA

LIP

S C

HE

CK

OU

T; V

erif

ies

func

tiona

l pe

rform

ance

of t

he m

ain-

I N

AR

1 stage

cal

ips

switc

hes

ar

elat

ed c

ircu

itry

.

QA

PD

G

DC

-26

S-l

l P

RO

PE

LLA

NT

DIS

PE

RS

ION

SY

ST

EM

FU

NC

TIO

N T

ES

T;

Ver

ifie

s th

at,

wit

h I W

AR

/ the pro

per

stim

uli,

the

prop

ella

nt d

ispe

rsio

n sy

skem

fun

ctio

r~s p

rope

rly.

QA

PL

I

GD

C-2

6 1 S

-ll

PA

NE

L L

AM

P S

EQ

UE

NC

ING

; S

eque

nces

the

pan

el l

amps

. I

QA

PO

G

DC

-26

S-l

l B

US

PO

WE

R O

N;

Brin

gs ~

p S

-ll

stag

e po

wer

afte

r ch

ecki

ng s

wit

ch a

nd h

ardw

are

/ NA

R

1 configu

ratio

n.

Ver

ifies

bur

lev

els

to b

e w

ithi

n to

lera

nce

and

scan

s st

age

disc

rete

sta

tus.

S-l

l P

RE

SS

UR

IZA

TIO

N C

OM

PO

NE

NT

S C

HE

CK

OU

T; V

erifi

es p

re-t

est

conf

igur

atio

n an

d fu

nctio

nal

perfo

rman

ce o

f LO

X &

LH

2 v

ent

valv

es,

and

the

23

psi

a an

d ta

nk h

igh

pres

sure

sw

itche

s.

S-l

l P

RO

PE

LLA

NT

UT

ILIZ

AT

ION

SY

ST

EM

FU

NC

TIO

NA

L;

Ver

ifies

PU

sys

tem

te

mpe

ratu

re l

evel

s an

d st

abilf

ty;

veri

fies

brid

ge s

lew

ope

ratio

n,

and

veri

fies

MR

CV

co

ntro

l lo

gic.

PA

S2

I G

DC

-26

S-I

l/SW

ITC

H

SE

LEC

TO

R F

UN

CT

ION

AL;

Ver

ifie

r ca

pabi

lity

of r

ecei

ving

and

N

AR

ve

rify

ing

rece

ipt,

and

of i

ssui

ng S

-ll

com

man

ds.

QA

SP

G

DC

-26

S-I

I/S

EP

AR

AT

ION

S

YS

TE

M F

UN

CT

ION

AL;

V

erifi

es t

hat

the

syst

em w

ill,

upon

N

AR

co

mm

and

from

the

IU

(via

the

5-1

1 sw

itch

sel

ecto

r),

prov

ide

the

follo

win

g or

dnan

ce

func

tions

: S

-ll

ordn

ance

arm

, S

-ll

seco

nd p

lane

sep

arat

ion,

S-

111'

s-IV

B or

dnan

ce a

rm,

and

S-I

I/S

-IV

B

sepa

ratio

n an

d re

tro

rock

et f

ire.

A

lso,

it v

erifi

es p

rope

r E

BW

firi

ng

unit

resp

onse

to

thes

e co

mm

ands

.

I I

FO

RM

16-

22d

(RE

V.

5 6

9)

i-

Page 36: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t Pr

ogra

ms

(Con

tinue

d)

Page 37: JOHN F. KENNEDY SPACE CENTER

NA

SA

AU

TW

. E

LEM

EN

T A

ND

lV

AR

R

ES

PO

NS

IBLE

C

ON

TR

AC

TO

R

G3

C4

/ BA

TC

VA

LL

G

DC

4

EA

TC

VA

MC

IN

S-2

1

BA

TC

GD

C-2

1 BAT

C

VA

RS

G

DC

4

BA

TC

VA

RY

G

DC

-4

BA

TC

I F

OR

M 1

4-22

6 (R

EV

. 5

/69

Tab

le 1

-4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Cvn

tinue

d)

PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

LIN

KIN

G P

RO

GR

AM

FO

R C

OU

NTD

OW

N;

Pro

vide

s lin

king

of

all

pro

gram

s (w

here

po

ssib

le)

and

no

r~n

illy

run

betw

een

appr

oxim

atel

y T-

9 ho

urs

and

T-1

hou

r an

d 5

1 m

iri.

I ! IxiX

LI

NK

ING

PR

OG

RA

M F

OR

OV

ER

ALL

TE

ST

S;

Link

s a

ll p

rogr

ams

and

perfo

rms

pro-

ce

dura

l fu

nctio

ns b

etw

een

T-1

hou

r 5

0 m

inut

es a

tid T

-27

rni

,iute

s;

oper

atio

nally

lin

ks

VA

TS

to

T-0

.

RA

CS

RA

PID

CO

NT

RO

L B

AC

KU

P;

Issu

es R

AC

S c

omm

ands

, as

req

uire

d,

for

HI,

LO

or

RU

N to

any

sta

ge (

S-I

C,

S-1

1,

S-I

VB

, or

IU

), or

all

sta

ges.

ME

AS

UR

ING

SY

ST

EM

RA

PID

RA

CS

CA

LIB

RA

TIO

N;

Issu

es a

ll s

tage

s,

all

RA

CS

- H

IGH

, LO

W,

and

RU

N.

OW

S S

WIT

CH

SE

LE

Cl O

R T

ES

T;

Tes

t w

ill

issu

e a

ll O

WS

swit

ch s

elec

tor

clia

nnel

s,

in th

e tru

e,

thes

in

the

com

plim

ent

form

.

LV/I

NT

EG

RA

TE

D P

OW

ER

TR

AN

SF

ER

; C

heck

s th

e ex

tern

al b

us v

olta

ges

and

sub-

se

quen

t to

pow

er t

rans

fer,

ch

ecks

the

int

erna

l bu

s vo

ltage

s,

flagg

ing

any

out-

of-

tole

ranc

e vo

ltage

s w

ith

appr

opria

te e

rror

mds

sage

s.

RA

NG

E S

AF

ET

Y P

RO

GR

AM

; C

heck

s E

BW

cir

cuit

s, t

he r

ange

saf

ety

syst

elns

, an

d m

onito

rs w

hen

SR

O is

sues

cut

off.

RE

CY

CLE

PR

OG

RA

M;

Rec

ycle

s to

T-2

2 m

inut

es,

VA

MC

run

as

part

of

recy

cle.

X

X X

O

ther

NA

SA

Aut

h.

51

2/

I / I El

em:

GD

C-3

1

51

3

X 1 X

I X

1 Li

nked

by

VA

TS

,

/ / V

AR

Y,

VA

LJ

X X

X

Link

ed b

y V

AL

L

/512/

1 1 al

id V

AL

J 1513

X

X X

Link

ed b

y V

AL

L,

VA

LK,

'JA

W

Oth

er N

AS

A A

uth.

E

lem

: G

DC

-3

X X

X

I

Page 38: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

4.

Sat

urn

V O

pera

ting

Sys

tem

and

Tes

t P

rogr

ams

(Con

tinue

d)

-

-

I V

AS

S

VA

TC

VA

TS

VA

VS

WA

CR

WA

ES

1 W

AP

O

WA

PX

I

WA

SL

I i

,-2%

(R

EV

. 3

/69

)

AU

TW

. F

OR

V

E~

~C

L,

NO

.

51

21

ST

AT

US

AN

D/O

R R

EM

AR

KS

1

NA

SA

AU

TU

. E

LE

YE

NT

4N

0

RE

SP

ON

SllL

E

CO

NT

RA

CT

OR

VZ

DS

, an

d V

ZF

1

PR

OG

RA

M T

ITL

E &

FU

NC

TIO

N

? O

0

51

3

GD

C-2

B

AT

C

Lfi

S

WIT

CH

SE

LEC

TO

R I

NT

ER

FA

CE

TE

ST

; P

rovi

des

an i

nter

face

che

ck o

f th

e L/

V

switc

h se

lect

or b

y st

age.

INT

ER

FA

CE

X

8 WW

INS

-12

B

AT

C

GD

C-4

B

AT

C

GD

C-2

B

AT

C

GD

C-2

4 B

AT

C

ME

C-2

3

BA

T C

GD

C-2

4 B

AT

C

GD

C-2

4 B

AT

C

CD

C-2

B

AT

C - -

d ..-=

; X

L/V

TE

LE

ME

TR

Y C

ALI

BR

AT

ION

; P

rovi

des

auto

mat

ic c

alib

ratio

n se

quen

ce.

TE

RM

INA

L S

EQ

UE

NC

E P

RO

GR

AM

; P

rovi

des

linki

ng o

f a

ll th

e pr

ogra

ms

run

betw

een

T-2

4 a

nd T

-0 m

inut

es,

and

auto

mat

ical

ly p

erfo

rms

proc

edw

al f

unct

ions

dur

ing

this

tim

e pe

riod.

L/V

SIM

ULA

TE

D F

LIG

HT

PR

EP

S;

Issu

es s

elec

ted

MD

Os

and

cl~

eck

s for

prop

er

resp

onse

.

S-IC

CU

TO

FF

RE

LA

YS

TE

ST

; V

erifi

es p

rope

r op

erat

ion

and

resp

onse

s o

f S

-IC c

utof

f se

nsor

s fo

r th

rust

-not

-k

cub

ff,

LOX

and

fue

l de

plet

ion

cuto

ff,

cuto

ff o

f ad

jace

nt

engi

nes;

an

d ch

ecks

the

redu

ndan

cy o

f a

ll c

utof

f ci

rcui

try.

F-1

EN

GIN

E S

EQ

UE

NC

E T

ES

T;

Ver

ifies

cor

rect

ope

ratio

nal

sequ

ence

and

res

pect

ive

allo

wab

le t

ime

limit

s of

the

F-1

eng

ine

valv

e t

imin

g.

S-IC

D

AIL

Y P

OW

ER

ON;

R

ovi

de

s tk

cap

abili

ty o

f ap

plyi

ng p

ower

to

the

S-IC

ES

E

and

stag

e.

S-IC

PO

WER

TR

AN

SF

ER

FU

NC

TIO

NA

L;

Ver

ifies

S-IC

pw

er

tran

sfer

cir

cuitr

y,

rapi

dly

and

relia

bly,

pri

or to

LV

and

SA

I ove

rall

test

.

S-I

C S

WIN

G A

RM

PR

ES

SU

RE

& L

EV

EL;

C

heck

s op

erat

ion

of S

/A E

SE

by

hlee

ding

do

wn

hydr

aulic

pre

ssur

e in

the

actu

ator

s an

d ch

ecki

ng f

or E

SE

low

lev

el s

ensi

ng a

nd

repl

enis

h.

ii

gs

z

Sub

pro

gram

s W

ZIT,

Q

ZIT

,XZ

IT

,KZ

IT,

X X X X X

X

<o

uf

9P

O3

X

X

X

X

X

X

X

X

Lin

ked

by

VA

LL

, V

AR

Y,

VA

W

Oth

erN

AS

AA

uth

Ele

G

DC

-3

VZ

T S,

V

ZT

T,

VZ

TM

, V

ZG

T

subr

outin

e V

MT

S

1 Li

nked

by

VA

LL

and

V

AR

Y.

Sub

pro

gram

Link

ed b

y V

AT

S

Sub

pro

gram

s W

ZCR

, an

d W

ZR

B -

(WZC

R

is li

nked

by

WA

SV

Sub

pro

gram

WZ

PO

L

inke

d b

y V

AL

J

Link

ed b

y W

AS

V

Link

ed b

y V

AL

L;

Oth

er N

AS

A A

uth

Ele

m \/

ME

C-1

1

X fa

C1

X

X X

X X X X X

X

X X X

I X X X X

X X

X

X

X

X

X

X X X

X X

I

Page 39: JOHN F. KENNEDY SPACE CENTER

c.'

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-2

2 B

AT

C

GD

C-2

B

AT

C

ME

C-3

3

BA

TC

GD

C-2

4 B

AT

C

GD

C-2

B

AT

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3

I

lVA

R

WA

SP

WA

SS

WA

ST

WA

SV

WA

TL

XA

DA

XA

DS

XA

EB

XA

EC

XA

lC

XA

HB

LKk

FO

RM

Tab

le 1

4. S

atur

n V

Ope

ratin

g S

yste

m a

nd T

est

Pro

gram

s (C

ontin

ued)

INT

ER

FA

CE

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

N

O.

SW

ING

AR

M P

OW

ER

UP

; S

cans

all

sw

ing

arm

sw

itche

s an

d in

dica

tions

dur

in!,

syst

emat

ic p

ower

up

of t

he s

yste

m.

S-I

C

SW

ITC

H S

ELE

CT

OR

TE

ST

; V

erifi

es p

rope

r re

spon

se t

o th

e S

-IC

sw

itch

sele

ctor

com

man

ds w

;th b

oth

stag

e bu

ses

or e

ither

bus

on.

S-I

C

PN

EU

MA

TIC

CH

EC

KO

IIT R

AC

K S

WIT

CH

TE

ST

; P

rovt

des

chec

kout

of

the

pile

umat

ic r

acks

and

rec

ordi

ng u

i the

~ie

cess

ary d

ata

for

real

tin~

e ana

lysi

s.

S-I

C

OA

T P

RE

PS

; .'e

rifie

s th

e st

atus

of

vario

us S

-IC

stay

e el

ectr

onic

sub

syst

enis

.

S-iC

T

AIL

SE

RV

ICE

MA

ST

PR

ES

SU

RE

& L

EV

EL;

C

heck

s op

erat

ion

of T

SM

ES

E h

y bl

eedi

ng d

own

ISM

hyd

raul

ic p

ress

ure

and

chec

king

for

ES

E l

ow l

evel

sen

sing

and

re

plen

ish.

S-IV

B

DD

AS

AU

TO

MA

TIC

SC

AN

; P

rovi

des

auto

mat

ic c

heck

out

of i

ndiv

idua

l DD

kS

inea

sure

mer

its o

n S

-IV

B s

tage

.

S-IV

B

CO

UN

TDO

WN

Dls

,RE

TE

SC

AN

; V

erifi

es t

he S

-IV

B d

iscr

ete

base

line

ai

crit

ica

l tim

es.

S-I

VB

E

BW

TE

ST

; P

rovi

des

capa

bilit

y to

ver

ify o

pera

tion

of E

m

asso

ciat

ed w

ith

UR

igni

tion

and

UR

jett

ison

ord

~ia

nce fu

nctio

ns.

S-I

VB

E

NG

INE

CO

NT

RO

L A

SS

Y F

UN

CT

ION

AL,

E

NG

INE

CO

MP

ON

EN

T &

LA

DD

ER

T

ES

T;

Fun

ctio

nally

ver

ifies

the

eng

ine

cont

rol

asse

mbl

y by

ctw

ckin

g th

e en

gine

la

dder

fun

ctio

ns a

nd c

utof

f lo

gic.

V

crifi

es e

nq

i~e

com

pone

nt t

est a

nd e

ngin

e la

dder

fu

nctio

ns a

re o

pera

tiona

l.

S-IV

B

INIT

IAL

CO

ND

ITIO

N S

CA

N;

Ver

ifies

pre

pow

er s

can,

gro

und

pow

er s

can,

an

d ve

hicl

e po

wer

sca

n fo

r pr

oper

con

figur

atio

n.

S-IV

B E

SE

HIG

H B

AY

QU

ALI

FIC

AT

ION

; V

erifi

es S

-IVB

ES

E h

igh

bay

prio

r to

M

DA

C

1 vehi

cle

stac

king

.

t&Z

W (

RE

V.

5 6

9)

x x

x x

x I

Link

ed b

y V

AL

J 5

12

/-

I 5 1.3

X,

X

X

X,

X X

X

Ele

rn:

ME

C-1

2

XZ

MM

1 I I I

X

X

X

X

Link

ed b

y X

AP

S

Sub

prog

ram

XZ

lC

X

X

X

X

X

Link

ed b

y X

AP

L

and

calls

17

Sub

- pr

ogra

ms.

Page 40: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

4.

Sat

urn

V O

pera

tinq

Sys

tem

and

Tes

t P

rogr

ams

I

NA

SA

AU

TH

. ~

EL

EY

LN

T AN

D

RC

SP

ON

SIO

LE

I C

WT

RA

CT

OR

I

PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

INS

-21

S

-IV

B E

NG

INE

& A

PS

ME

AS

UP

EM

EN

T C

ALI

BR

AT

ION

CH

EC

KS

; S

cans

spe

cifie

d M

DA

C

mea

sure

men

ts w

ith s

peci

31 c

alib

ratio

n da

ta,

aver

age

the

read

ings

and

com

pare

aga

inst

sp

ecifi

ed l

imits

.

ME

C-2

4

S-I

VB

PR

OP

ULS

ION

CH

EC

KS

; C

heck

s th

e fu

nctio

n an

d tim

ing

of p

ropu

lsio

n va

lves

, M

DA

C

auto

mat

ical

ly c

alls

NTD

R t

o c

heck

dis

cret

e re

spon

se ti

min

g.

Mak

es f

unct

iona

l ch

eck

of S

-IV

B p

ress

ure

switc

hes.

GD

C-2

3 S

-IV

B P

OW

ER

DIS

TRIB

UTI

ON

; V

erifi

es a

ll p

ower

dis

trib

utio

n an

d co

ntro

l sw

itchi

ng

MD

AC

ci

rcui

ts;

for

vehi

cle

and

ES

E.

GD

C-2

3 S

-IV

B

PR

EP

S A

ND

FU

NC

TIO

NA

L;

Fun

ctio

nally

che

cks

S-I

VB

sys

tem

s re

quire

d to

I I M

DA

C

1 suppor

t ov

eral

l tes

ts th

roug

h F

RT

.

XA

PL

XA

PS

XA

PU

XA

PX

XA

RS

XA

SS

XA

UE

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

GD

C-2

3 M

DA

C

M E

C -2

4

MD

AC

S-I

VB

PA

NE

L L

AM

P T

ES

T;

Ver

ficat

ion

of l

amps

on

MD

AC

S-I

VB

pan

els

by c

yclin

g

disc

rete

s w

ith

man

ual i

de

niif

icd

ion

. S

-IV

B P

OW

ER

SE

TUP

; P

rovi

des

a se

quen

tial

pow

er tu

rnon

and

tur

noff

for

the

vehi

cle

subs

yste

m a

nd s

tage

int

egra

ted

test

.

/ S-N

B P

OW

ER

TR

AN

SF

ER

; F

unct

iona

ily v

erifi

es t

he S

-IV

B p

ower

tran

sfer

cir

cuitr

y.

S-I

VB

R

AN

GE

SA

FE

TY

FU

NC

TIO

NA

L T

ES

T;

Sem

iaut

3mat

ical

ly d

eter

min

es t

he

oper

atio

nal c

apab

ility

of

crit

ica

l el e

m e

n'.^

of t

he R

ange

Saf

ety

Sub

syst

em.

I S-I

VB

SW

ITC

H S

ELE

CT

OR

RE

SE

T;

Res

ets

the

S-I

VB

sw

itch

sele

ctor

fun

ctio

ns a

fter

an in

put

has

been

mad

e.

S-I

VB

ULL

AG

E E

NG

INE

FIR

ING

TE

ST

; V

erifi

es p

rope

r fir

ing

and

cham

ber

pres

sure

s of

the

S-I

VB

eng

ines

.

*N/A

C

AP

-A

SA

TU

RN

V O

PS

YS

; C

ontr

ols

and

exec

utes

Lau

nch

Veh

icle

Tes

t an

d M

onito

r P

rog

ra~

s

71

/ ! eithe

r un

der t

he a

utom

atic

lin

kin

g c

apab

ility

of

AT

OL

L o

r up

on i

ndiv

idua

l req

uest

s fro

m

*MS

FC

D

eliv

ered

Pro

gram

Page 41: JOHN F. KENNEDY SPACE CENTER
Page 42: JOHN F. KENNEDY SPACE CENTER

- - - .-

- - - - -- - --

- -

X

X

X

X X

X

X

XX

XX

XX

-- ~

- - .~

. .. .

...

le3!Jls13 A7

X

w"t'43 3'83 A

7 x

xx

xx

x

x

X

dn

va

A/S p

al uo! ~

e~

~s

uo

ua

a

XX

X

X X

w

X

X

X

..

I-

--

-

. --

-- --

. -

_

.-P

.

XX

X

X

X X

X

X X

X

X

Page 43: JOHN F. KENNEDY SPACE CENTER

---

--

.~

-

X X

X

X

X

X

X

XX

XX

XX

X

X

X

-

.. . -.

-

. ~

.. -

-

. . .- . -

-

X

X

X

X

X

X

XX

XX

XX

XX

X

X

--

--

-A

-

--.

- .

-- --

- -

X

X

X

X X

X

-~

~

-

-- .

-. .

- --

- --

-. . . --

. - .- .- -.

-

- .- .

. - -~

.- -. --

- -

- X

X

X

X

X

X

X

XX

X

X

-- -p

. ---

-

---

-. --

-----

X

X

X

-- -

- A -.

--

~

. . - - ---

X

X

X

X

XX

XX

X

--.

-.

- .-

- ~

...-

--

X

X

XX

XX

X

-

- .-

-

- -

- ..

- - .

. -. . . . . .

----

-.

-- .-

-

X X

X

X

X

XX

X

X

X

X

X

XX

XX

X

X

XX

XX

X

-.

------

X X

x

xx

xx

xx

X

XX

XX

XX

XX

XX

X

X

-

- - -. . --

--

Laun

ch C

ount

dow

n -.

-

. - - - -

--

Cou

ntdo

wn

Dem

onst

ratio

n T

est

SA

I Bac

k U

P G

uida

nce

Tes

t F

light

Rea

dine

ss

Tes

t --

L

V F

light

Sys

tem

s R

edun

danc

y T

est

-

S/V

OA

T N

o. 1

( P

luas

In)

SN

Ele

ctri

cal M

ate

I

Mal

func

tion

OA

T

LV G

&C C

heck

s

LV

Ele

ctri

cal

Sys

tem

s T

est

LV

Sta

ge o

r S

ub-s

yste

m

Page 44: JOHN F. KENNEDY SPACE CENTER

Table 1-5. Saturn V Ma; ?st Program Matrix (Continued)

Page 45: JOHN F. KENNEDY SPACE CENTER

X

X

X

--

- ~

XX

XX

XX

XX

X

XX

X

X La

unch

Cou

ntdo

wn

. -- . .. - --

.

Coun

tdow

n D

emon

stra

tion

Test

S

AI B

ack

Up

Gui

danc

e Te

st

Flig

ht R

eadi

ness

Te

st

LV

Flig

ht S

yste

ms

Red

unda

ncy

Test

S

AI O

AT

No.

1

(Plu

gs I

n)

SAI E

lect

rica

l M

ate

LV S

win

g An

n O

AT

~alf

un

ctio

n OA

T

LV

G&

C C

heck

s

LV

Ele

ctri

cal

Syst

ems

Test

L

V S

tage

or

Sub-

Syst

em

Page 46: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-6.

Oth

er S

atur

n V

Ope

ratin

g S

yste

ms

and

Tes

t P

rogr

ams

*AT

GT

DD

TG

DT

Ol

DT

02

DT

12

DT

13

LIE 0

4

DE

07

DT

14

DE

05

I

DT

15

DE

06

nA

u u

rn.

ELeM

CNr A

ND

R

ES

PO

NS

IBLE

C

ON

TR

AC

TO

R

CA

P-A

IBM

CA

P-A

IB

M

GD

C-2

7/3

1

IBM

IN S-1

3 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GO

C-3

1 IS

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IS

M

GD

C-3

1 IB

M

GD

C-3

1 IS

M

226

RE

V.

5/6

(

*MS

F C

Del

iver

ed p

rogr

am

AU

TM.

FO

R

YE

HIC

L~

N

O.

51

2/

51

3

PRO

GRA

M T

ITL

E 6

FU

NC

TIO

N

AT

OL

L T

AP

E G

EN

ER

ATO

R (

AT

OLL

UT

ILIT

Y);

P

rovi

des

the

capa

bilit

y to

upd

ate

the

AT

OL

L d

rum

ind

ex.

DIS

PLA

Y D

ES

CR

I PTI

ON

TA

PE

GE

NE

RA

TOR

; G

ener

ates

Dis

play

Des

crip

tion

tape

fro

m s

ymbo

lic in

puts

.

SGC

C G

MT

MA

INT

EN

AN

CE

TE

ST;

Exe

rcis

es th

e op

erat

ion

of t

he G

MT

cloc

k,

whi

le

runn

ing

unde

r the

con

trol

of

the

Sat

urn

oper

atin

g sy

stem

(B

HC

).

SGC

C D

DA

S C

UR

SO

RY

TE

ST;

P

rovi

des

a cu

rsor

y te

st o

f th

e D

DA

S IO

DC

and

com

pute

r in

terf

ace

unit.

RC

A-l

lOA

/DD

P-2

24

IN

TE

RF

AC

E C

HE

CK

OU

T; P

erfo

rms

an o

n-lin

e ch

ecko

ut o

f th

e R

CA

-11O

A I

OD

C-6

and

the

OD

P-2

24 f

ully

buf

fere

d ch

anne

l and

ind

icat

es m

alfu

nctio

n.

LCC

INS

TR

UC

TIO

N T

ES

T;

Ver

ifies

tha

t al

l but

the

I/O

and

som

e co

ntro

l op

code

s pe

rform

pro

perl

y .

ML

C IN

ST

RU

CT

ION

TE

ST

, P

AR

T 1;

Ver

ifies

tha

t a

ll b

ut t

he I

/O a

nd s

ome

cont

rol o

p co

des

perfo

rm p

rope

rl y .

ML

C IN

ST

RU

CT

ION

TE

ST

, P

AR

T 2

; V

erifi

es t

hat

all

but t

he I /O

an

d so

me

cont

rol o

p co

des

perf

om, p

rope

rly fo

r th

e LC

C.

LCC

DR

UM

TE

ST;

Ver

ifies

, in

less

than

cer

tain

test

, th

at d

ata

can

be t

ran

sfe

r~d

t.0

and

from

the

dru

m.

MLC

DR

UM

TE

ST;

V

erifi

es,

in le

ss th

an c

erta

in te

st,

that

dat

a ca

n be

tra

nsfe

rred

to

and

from

tk

drum

.

LCC

ME

MO

RY

TE

ST;

P

erfo

rms

a cu

rsor

y ch

eck

of H

SM

.

ML

C M

EM

OR

Y T

ES

T;

Per

form

s a

curs

ory

chec

k of

HS

M fo

r th

e LC

C.

ST

AT

US

AN

D/O

R

RE

MA

RK

S

2 o

0

z

X .n

0

INT

ER

FA

CE

8 ",,a

<4

"5

5z

;g

*

oE

;2

:;

"

I I

Inte

rrel

ated

w/D

T13

Inte

rrel

ated

w/D

T13

Inte

rrel

ated

w/D

T 1

4

Inte

rrel

ated

w/D

T15

(

XX

X

XX

2 r

Za

y

X X X

XX

X X

X X X

X X X X

X

X

X X X

X

X

Page 47: JOHN F. KENNEDY SPACE CENTER

IVA

R

DT

P2

DT

SC

OT

23

EN

RS

TU

Ol

. IA L

T

JAW

N

*MU

01

*NT

94

*NT

97

WT

98

qT

99

limm

m

WS

FC

I

Tab

le 1

-6.

Oth

er S

atur

n V

Ope

ratin

g S

yste

ms

and

Tes

t P

rogr

ams

(Con

tinue

d)

1 I

INT

ER

FA

N

AS

A A

UT

H.

ELE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

56

5

<n

u

INS

-13

I D

DA

S C

UR

SO

RY

TE

ST

. I

I Ix

LCC

ON

-LIN

E

PE

RIP

HE

RA

L E

QU

IPM

EN

T T

ES

T;

Prin

ter,

tap

e st

atio

ns 1

-3,

& 2

-9

card

rea

der.

///I

(

IBM

GD

C-3

1 IB

M

LCC

SE

LF-C

HE

CK

; M

onito

rs th

e pe

riphe

ral e

quip

men

t with

in th

e LC

C to

det

erm

ine

its

oper

atio

nal

stat

us.

LV

TE

RM

INA

L C

OU

NT

SIM

ULA

TIO

N;

Issu

es L

DO

s fro

m T

-24

to

T+

3 m

inut

es f

or

BA

T C

I L

V c

ount

dow

n op

erat

or tr

aini

ng.

I ixx1 i

GD

C-3

1 C

AP

-5

GD

C-3

2 IB

M

S-IC

T

ER

MIN

AL

CO

UN

T S

IMU

LATI

ON

; Is

sues

LD

Ds

from

T-1

5 t

o 1

-0 m

inut

es f

or

aAT

C

GD

C-2

4 I th

e S

-IC s

tage

to

trai

n pa

nel o

pera

tors

. I IX

IX/ I

MLC

SLO

W S

YS

TE

M R

EC

OV

ER

Y B

OO

T S

TRA

P;

Load

s M

LC U

XE

X L

oade

r-M

odifi

er

from

MLC

MT

S 1

-3 o

r 2

-3 (

desi

gned

for

rem

ote

auto

mat

ic s

low

sys

tem

rec

over

y).

SIM

ULA

TE

D P

LUS

-TIM

E

TA

BLE

GE

NE

RA

TOR

TE

ST;

R

uns

valid

ity c

heck

s on

a

sim

ulat

ed p

lus+

ime

card

dec

k fo

r ei

ther

tow

er t

est,

stat

ion

acqu

isiti

on,

or c

omm

and

func

tions

; w

rites

dec

k.

INS

-2 1

DIS

CR

ET

E A

CT

IVIT

Y M

ON

ITO

R T

ES

T;

Pro

vide

s th

e st

atus

and

num

ber o

f L

Dls

and

IS

M

CA

P-A

I VD

ls n

ot i

n a

pre

spec

ified

sta

te f

or o

ne o

r all

sta

ges.

II

III

CA

P-A

IB

M

CA

P4

( L/

V S

WIT

CH

MO

NIT

OR

& I

NIT

IALI

ZA

TIO

N;

Dis

play

s an

d pr

ints

the

stat

us o

f a

ll V

Dls

IB

M

and

SD

ls.

I I I lX

iX

ME

AS

UR

EM

EN

TS

PR

E-P

RO

CE

SSO

R;

Gen

erat

es R

AC

S m

easu

rem

ents

dat

a ta

bles

for

use

by th

e D

DA

S R

AC

S C

alib

ratio

n P

rogr

am.

. .

UC

C R

EM

OTE

LO

AD

/UN

LOA

D;

Dis

play

con

trol

com

pute

r loa

d7un

load

pro

gram

resp

onds

to

dis

aete

s in

itiat

ed fr

om d

iscr

ete

pane

l, an

d ei

ther

rel

oads

the

DC

C o

r du

mps

the

DC

C

on p

rinte

r or

log

tape

. i

CA

P-A

IS

M

ST A

TUS

AN

D/O

R

RE

MA

RK

S

L/V

AC

TIO

N T

AB

LE U

PD

ATE

; P

rovi

des

the

capa

bilit

y to

mod

ify,

on li

ne,

the

Dis

cret

e A

ctio

n Ta

ble.

AU

TH

. F

OR

V

EH

ICL

E

NO

.

., x

x

E I = rf

X

X

X

X

X X

X X

Inte

rrel

ated

W/D

T02

st

21

513

5

an

0

X

xx

x

X

X

xx

x

xx

x

X X

Link

ed b

y V

AL

L

OF

F-L

INE

on1

y

OF

F-L

INE

onl

y

Page 48: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-6.

Oth

er S

atur

n V

Ope

ratin

g S

yste

ms

and

Tes

t P

rogr

ams

(Con

tinue

d)

I N

AS

A A

UT

H.

-I

i--

CO

NT

RA

CT

OR

P

RO

GR

AM

TIT

LE

b F

UN

CT

ION

*NT

DR

*SE

89

I C

AP

-A

I ALT

ER

NA

TE

ME

MO

RY

CH

EC

KE

R.

IBM

*SE

88

CA

P-A

IB

M

* ST

91

C

AP

-A

RE

CO

VE

RY

DU

MP

RE

TR

IEV

AL;

P

rovi

des

the

capa

bilit

y to

log

the

ML

C li

illar

y du

rtlii

1 1 1

I IBM

I on

log

tape

, an

d pr

esen

t re

cove

ry a

nd t

ile s

yste

m s

tatu

s.

I i

LN

DIS

CR

ET

E R

ES

PO

NS

E T

IME

; M

easu

res

the

elap

sed

time

betw

een

the

issu

ance

of

MD

O a

nd M

DI,

or,

DD

AS

dis

cret

e ta

lkba

ck.

CA

P-A

IB

M

* ST

90

AN

ALO

G T

ES

T P

OIN

T M

ON

ITO

R;

Mon

itors

a m

axim

um o

f th

ree

spec

ific

har

dwire

an

alog

tes

t po

ints

per

exe

cutio

n cy

cle,

an

d di

spla

ys e

ach

anal

og v

alue

rea

d (k

eybo

ard

entr

y m

ust

be m

ade

for

each

tes

t po

int t

o be

mon

itore

d).

Upd

ates

for

bia

s, s

igna

l ra

nge,

an

d de

scri

ptio

n m

ay b

e en

tere

d.

SE

88

may

als

o be

use

d to

del

ete

an a

ctiv

e ar

~al

og sl

ot

from

the

mon

itor

tabl

e.

Con

trol

of

the

rout

ine

is v

ia t

he d

ispl

ay c

onso

le k

eybo

ard.

CA

P-A

IB

M

*ST

95

I !

Rsc

ronv

16.

226

(RE

V.

5/6

9)

ML

C R

EC

OV

ER

Y C

ON

TRO

L;

Tf~

is pm

grar

n is

the

cont

rolli

ng p

rogr

am f

or M

LC S

yste

m

Rec

over

y (S

SR

P)

Opt

ions

, by

allo

win

g ei

ther

sta

rtin

g o

f th

e re

cove

ry p

roce

ss o

r te

rmin

a tio

n.

If re

cove

ry i

s s

tart

ed,

the

prog

ram

d~

spla

ys tu

tori

al m

essa

ges

to s

tart

rec

over

y at

th

e M

LC.

The

LC

CC

is

set

to

DO

WN

sta

tus,

an

d in

terr

upts

are

inh

ibite

d.

tions

wit

h th

e M

LC

Sys

tem

Rec

over

y ar

e th

en b

egun

.

*%93

CA

P-A

I B

M

CA

P-A

I D

ISC

RE

TE

MA

SK

NN

MA

SK

RO

UTI

NE

; M

odifi

es,

by m

aski

ng o

r un

mas

king

, th

e IB

M

inte

rrbp

t co

ntro

l w

ord

grou

ps.

It a

ccep

ts d

ata

whi

ch w

ill

mod

ify t

he L

CC

C o

r M

LC

1

dis

c~e

te mon

itor

inte

rrup

t (M

I) c

ontr

ol w

ords

. If

a g

roup

is

mas

ked,

an

y ch

ange

in

Dl

stat

ks c

anno

t ca

use

an i

nter

rupt

. If

the

grou

p is

unm

aske

d,

an i

nter

rupt

can

be

allo

wed

ML

C R

EM

OT

E L

OA

D;

Init

iall

y lo

ads

the

ML

C O

pera

ting

Sys

tem

fro

t?~ th

e L

CC

C s

yste

m

Mas

ter

Tape

, to

allo

w p

atch

ing

of M

LC

cor

e an

d dr

um r

esid

ent p

rogr

ams,

an

d to

loa

d fu

nctio

n ex

ecut

or b

inar

y ca

rd d

ecks

.

I 1 w

hen

a D

l cb

anye

is

det

ecte

d,

All

dis

cret

e gr

oups

may

be

unm

arke

d w

ith

one

keyb

oard

Page 49: JOHN F. KENNEDY SPACE CENTER
Page 50: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-7.

Sat

urn

V O

pera

tiona

l D

EE

-6 P

rogr

ams

%SFC

Del

iver

ed P

rogr

am

ST

AT

US

AN

D/O

R

RE

MA

RK

S

AU

TM

. F

OR

Y

En

lCL

~

NO

.

51

2/

5I3

/ 2

06

f

PR

OC

RA

M T

ITL

E 6

FU

NC

TIO

N

OP

ER

AT

ING

SY

STE

M;

Pro

vide

s co

ntro

l to

loa

d an

d ex

ecut

e D

EE

-6 P

rogr

ams

and

acco

mpl

ishe

s a

ll W

cha

nnel

out

put.

SC

AN

PR

OG

RA

M - P

AR

T 1

; In

puts

dis

cret

e st

atus

cha

nges

from

the

Rem

ote

Sca

nner

, an

d re

cord

s th

ese

chan

ges

and

the

time

of o

ccur

renc

e on

var

ious

out

put

med

ia.

SC

AN

PR

OG

RA

M -

PA

RT

2;

Inpu

ts d

iscr

ete

stat

us c

hang

es f

rom

the

iie

mot

e S

cann

er,

and

reco

rds

thes

e ch

ange

s an

d th

e tim

e of

occ

urre

nce

on v

ario

us o

utpu

t m

edia

.

RE

MO

TE

SC

AN

NE

R O

PE

RA

TIO

NA

L P

RO

GR

AM

- PA

RT

1;

Load

s th

e R

emot

e S

cann

er

Ope

ratio

nal

Pro

gram

- P

art

2.

XD

S 9

30

RE

MO

TE

SC

AN

NE

R L

OA

DE

R/R

EC

OV

ER

Y P

RO

GR

AM

; Lo

ads,

pat

ches

, an

d du

mps

the R

emot

e S

cann

er c

ompu

ters

.

SC

AN

TA

BL

E G

EN

ER

ATO

R;

Con

stru

cts

the

Dis

cret

e ID

Tab

le M

atri

x fo

r a

spec

ific

Dis

cret

e ID

Tab

le.

OS

92

DU

MP

UT

ILIT

Y;

Sub

-rou

tine

of t

he O

pera

ting

Sys

tem

use

d to

dum

p th

e co

re

cont

ents

of

the

Rem

ote

Sca

nner

com

pute

r(s1

to th

e lin

e pr

inte

r an

d/or

mag

netic

tap

e.

OS

PA

TC

H U

TIL

ITY

; S

ub-r

outin

e of

the

Ope

ratin

g S

yste

m u

sed

to p

atch

thc

Col

e m

emor

y of

the

XD

S 9

30

com

pute

r.

OS

93

0 D

UM

P U

TIL

ITY

; S

ub-r

outin

e o

f th

e O

pera

ting

Sys

tem

use

d to

dum

p th

e co

re

-ont

ents

of

the

XD

S 9

30

com

pute

r to

the

line

prin

ter

and/

or m

agrie

tic t

ap

.

RE

MO

TE

SC

AN

NE

R O

PE

RA

TIO

NA

L P

RO

GR

AM

- PA

RT

2;

Det

ects

sta

tus

chan

ges

of 4

32

0 d

iscr

ete

inpu

t lin

es

from

a S

atur

n V

Veh

icle

and

tran

smits

th

is c

hang

e in

form

atio

n to

the

XD

S 9

30

com

pute

r vi

a a

H/S

Dat

a L

ink

for

subs

eque

nt p

roce

ssin

g.

FR

AN

KL

IN P

RIN

TE

R S

PIR

AL

TE

ST

; S

ub

iou

tin

e o

f th

e O

pera

ting

Sys

tem

use

d to

pr

int

a sp

iral

tes

t pa

ttern

on

all

stag

e pr

inte

rs.

lVA

R

*SC

61

*SC

62

*SC

63

*SC

64

*SC

65

*SC

66

*SC

67

*SC

68

* SC

69

*SC

70

*SC

71

INT

ER

FA

CE

I I j .. ..

.--..

- .-.

NA

SA

AU

TM

. E

LEM

EN

T A

ND

R

ES

PO

NS

IBLE

C

ON

TR

AC

TO

R

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IS

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

GD

C-2

7 IB

M

X

X

W6

a

f XX

X

X

*:

X X

X:

??

IK

An

n

"a

PO

0:

:;

XX

XX

I i

X

X

K

0,

-Z

WW

W

XX

X

XX

X

1

PI-"

^

X

XX

X

xixx

X X

X

Page 51: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-8.

Sat

urn

V D

DP

-22

4 D

ispl

ay O

PS

Y P

rogr

ams

*MS

FC

D

eliv

ered

Pro

gram

- NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

C

9N

TR

AC

TO

R

CA

P-A

IS

M

CA

P-A

IS

M

CA

P-A

IB

M

CA

P-A

IB

M

CA

P-A

IB

M

CA

P-A

IB

M

CA

P-A

IB

M

162% t

rav.

wrs

l

Fw

PRO

GR

AM

TIT

LE

6 F

UN

CTI

ON

CO

MM

ON

AN

D C

ON

SO

LE I

NP

UT

AN

ALY

SIS

; R

eads

in

and

pro

cess

es t

he i

nput

dat

a fro

m

the

cons

oles

.

DIS

PL

AY

DIA

GN

OS

TIC

RO

UTI

NE

; E

xecu

tes

diag

nost

ic t

ests

on

the

com

pute

r ,re

fresh

m

emor

ies

and

the

disp

lays

, an

d pe

riod

ical

ly c

heck

s th

e va

rious

err

or i

ndic

ator

s in

the

syst

em a

nd p

rove

s th

e er

ror

prin

tout

s on

the

com

pute

r ty

pew

riter

.

DA

TA

LIN

K R

OU

TIN

E;

Pro

vide

s a

mea

ns f

or t

wo-

way

com

mun

icat

ions

bet

wee

n th

e D

DP

- 22

4 C

ontr

ol C

ompu

ter

(DC

C)

and

the

Sat

urn

V R

CA

-1 IO

A c

ompu

ter.

DIS

PL

AY

AN

D P

ER

IPH

ER

AL

OU

TP

UT

RO

UTI

NE

; W

rite

s c'

ata

into

and

fro

m r

efre

sh

mem

orie

s, a

nd c

ontr

ols

the

oper

atio

n of

the

dig

ita

l sw

itch,

har

d co

py,

and

the

CC

TV

tr

ansm

itter

.

FO

RM

AT

TE

R R

OU

TIN

E;

Pro

cess

es a

nd f

orm

ats

all

dat

a re

ceiv

ed fr

om t

he R

CA

-11O

A

com

pute

r.

INP

UT

TR

AN

SLA

TO

R R

OU

TIN

E;

Tra

nsla

tes

Eng

lish

lang

uage

con

trol

sta

tem

ents

int

o co

mpa

ct m

essa

ges

for

the

RC

A-1

lOA

com

pute

r, an

d/or

pe

rform

s ce

rtai

n sp

ecia

l dis

play

co

ntro

l fun

ctio

ns.

DE

CU

AO

DC

TE

ST

RO

UTI

NE

S;

Per

form

s th

e ch

ecko

ut o

f th

e da

ta e

xcha

nge

cont

rol u

nit

(DE

CU

) an

d th

e in

put/o

utpu

t da

ta c

hann

el n

umbe

r 6 (

IOD

C 6

).

.

NO

TE: Th

e IN

TE

RF

AC

E a

nd A

UT

H f

or V

EH

ICLE

inf

orm

atio

n fo

r th

e pr

oclm

ms

liste

d

do n

ot a

pply

.

* IV

*R

*CC

* DF

* DN

*OQ

*Fo

*IV

.* LL

7nc

FO

RM

? - 0 0 A Z

ST

AT

US

AN

D/O

R

RE

MA

RK

S

See

Not

e

See

Not

e

See

Not

e

See

Not

e

Set

. Not

e

See

Not

e

See

Not

e

AU

W.

FO

R

NO

. V

)

a

I i 1 i Oa

o

w

sz

.

an

~~~i~~~

4n

u?

?.

"a

o0

!!

E%

+

A

Page 52: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions

DESCRIPTION

DISPLAY DCIC. NO.

523

5 24

525

526

527

5 28

529

53 0

53 1

532

533

534

53 5

53 6

53 7

538

539

54 0

541

542

543

544

545

546

547

548

KBC C O l Y I* 1 2 0

.- 8

I AUTHOR1 ZED FOR VEHICLE I

CALL, NO.

11

12

13

14

15

16

17

18

19

2 0

2 1

2 2

23

24

2 5

26

2 7

2 8

2 9

3 0

31

32

33

34

34

36

' R f V . # /ePI

REMARKS

NASA DISPLAY DESCRIPTION

OPERATIONS LIST CONSOLE 1

OPERATIONS L lST CONSOLE 2

OPERATIONS L lST CONSOLE 3

OPERATIONS L lST CONSOLE 4

OPERATIONS L lST CONSOLE 5

OPERATIONS L lST CONSOLE 6

OPERATIONS L lST CONSOLE 7

OPERATIONS L lST CONSOLE 8

OPERATIONS L lST CONSOLE 9

OPERATIONS L lST CONSOLE 10

OPERATIONS L lST CONSOLE 11

OPERATIONS L lST CONSOLE 12

OPERATIONS L lST CONSOLE 13

OPERATIONS L lST CONSOLE 14

OPERATIONS L lST CONSOLE 15

OPERATIONS L lST CONSOLE 17

SYSTEM CONFIGURATION

DDAS SYNC 81 CAL WORDS

DMON INSTRUCTION

DDAS INTERFACE CHECK, S-11, PART I

DDAS INTERFACE CHECK, S-Ill PART I1

DDAS INTERFACE CHECK, S-IC, PART I

DDAS INTERFACE CHECK, S-IC, PART II

DDAS INTERFACL: CHFLK, ESE, PART I

DDAS INTERFACE CHECK, ESE, PART II

Page 53: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

'

O i l P L I I DCSC. NO.

5 4 9

5 5 0

5 5 1

5 5 2

AUTHOR1 ZED FOR VEHICLE

CALL 1 NO.

3 7

38

3 9

4 0

5 5 3 1 5 5 4

5 5 5

5 5 6

5 5 7

5 5 8

5 5 9

5 6 0

5 6 1

5 6 2

5 7 7

5 78

579

5 8 0

5 8 1

5 8 2

583

5 8 4

5 8 5

5 8 6

* # C C O l U . # . la .

1 4 6

DESCRIPTION

DDAS INTERFACE CPECK, IU, PART I

DDAS INTERFACE CHECK, IU, PART II

DDASlNTERFACECHECK,S-IVB,PARTI

DDAS INTE,<FACE CHECK, S-IVB, PART II

IU REDLINES TCS 1

IU REDLINES TCS 2

IU REDLINES TCS 3

OPTIONS WHEN IN AUTO

OPTIONS WHEN IN SEMI MODE

VEHICLE MEASURING

CRITICAL LIMITS AT LIFTOFF

S-IC PRESSURE FUEL TANK ULLAGE

LONGITUDINAL ACCELERATION

ENGINE INLET LH2 TEMPERATURE

S-ll DISPLAY DESCRIPTIONS

S-II E+1, AND TEMPS-PG 1

S-ll GRND PNEUMATICS S 7 4 1 , UNIT -A

S-ll GRND PNEUMATICS 57-41, UNIT -0

S-ll GRND PNEUMATICS S7-41,UNITS C,D

S-ll STAGE PRESS SYSTEM

S-11 INT. DRY TEST DISCRETES

S-ll ENGINE SYSTEM

S-II ENGINE PUMP INLET TEMPS 81 pH.

S-ll SINGLE ENGINE MONITOR

S-11 LH RECIRC SYS DKCRETES

X X

X X

X

X

4 1

42

4 3

4 4

4 5

4 6

4 7

4 8

49

5 0

6 5

6 6

6 7

68

6 9

7 0

'71

72

7 3

7 4

I R I V # / * D l

X X

X X

X X

X X

X X

X

X

X

X

X

X

X

X

X

X

X

X

X X

X X

X X

X X

X X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

x

X

X

X

X

X

X

X

X

REMARKS

Page 54: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

DISPLAY DCSC. NO.

587

588

589

590

591

592

593

591

595

596

597

598

599

600

601

60 2

603

6 04

605

606

607

608

609

610

611

612

IIC wonu I* J P I

CALL NO.

75

76

77

78

79

80

81

82

83

84

85

86

87

88

89

90

91

92

93

94

95

96

97

98

99

100

~ n r v w a e i

DESCRIPTION

S-ll LOX RECIRC SYS DISCRETES

S-l l EAS MEASUREMENTS

S-11 PURGE AND VACUUM PRESSURE

S-11 FIRE & LEAK DETECTION

S-ll ENG TCH JACKET TEMPS

S- l l HEAT EXCH CONT (f)lSCRETES)

S-l l HEAT EXCH PURGUINERT (DISCRETES)

S-I1 HEAT EXCH ANALOGS

S-ll RECIRC SYS/HCL INJ/ACCUM F I L L

S-11 ENG LOX VLV DISCRETES

S-l l ENG LH2 AND GG VLV DISCRETES

S-l i E & I AND PU TEMPS (OAT)

S-l l E & I AND PU TEMPS (CDDT & LAUNCH)

S-I1 PROPELLANT LOAD

OPEN

S-II SYSTEMS READY

ENG MlSC PRESS

S-II MISC DISCRETES

S-l l MlSC TEMPS

S-ll MlSC PRESSURES AND TEMPS

5-11 OPEN

S- l l SYSTEM BY-PASS/BY-PASS INHIBIT, PAGE 1

S-ll SYSTEM BY-PASS/BY-PASS INHIBIT, PAGE 2

S-I1 PREPS COMPLETE, PAGE 1

S-l l PREPS COMPLETE, PAGE 2

S-l l PREPS COMPLETE, PAGE 3

REMARKS

I

1 -4 /

FOR

(V rc In

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

.Y

X

X

X

X

X

X

X

X

X

X

AUTHORIZED VEHICLE

m a

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

I X

X

X

X

X

don m r u ~

I

Page 55: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

DISCLAY DELC. NO.

613

614

615

C A L L NO.

101

102

103

DESCRIPTION

S- l l STAGE PRESS LIST

S-l l STAGE TEMP LIST

S- l l STAGE DISCRETE LIST A

616

617

I 641

642

643

644

645

646

647

648

649

650

651

652

653

654

655

656

657

* * C P O I U ,*.I.*

1-48

S-l l STAGE DISCRETE LIST B

GRD DDAS MEAS LIST

S-IVB DISPLAY DESCRIPTIONS - S-IVB HYDRAULIC SYSTEM

S-IVB PROPELLANT LOADING

S-IVB PROPLJI-S10N TERMINAL COUNT

S-IVB APS MODE

S-IVB POWER DISTRIBUTION

S-IVC! PREPS COMPLETE

S-IVB PREPS COMPLETE, APS, HYDR, MEAS, PU, AND HEX

S-IVB PREPS COMPLETE, PRESS RECIRC

S-IVB PREPS COMPLETE, ENGINE CO ORD

S-IVB READY LOGIC

S-IVB DAILY POWER SUPPORT

S-IVB DMON & SWITCH SELECTOR REF

BPTTERY MONITOR AND POWER TRANS. SUPPORT

S-IVB FUEL TANK He BTL REPRESS D20

S-IVB AMBIENT HELIUM SPHERE 0-236

S-IVB COLD HELIUM SPHERES 9-261

S-NB'G AND E SYSTEMS

I 104

105

121

130

131

132

133

134

135

136

137

138

139

140

141

142

143

144

145

,I*" *,*.I

REMARKS

FOR

N 4 In

X

X

X

GRAPH

GRAPH

GRAPH

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X I X

AUTnORIzED VEHICLE

m a

X

X

X

A D 9 r n N 3

X

X

X X

X X

X X

X X

X X

X X

X X

X

X

X X

X X

X

X X

X

X

X

X

X

X

X

X X X

Page 56: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

IU DISPLAY DESCRIPTIONS

DISPLAY DLSC. No.

7 0 8

7 1 0

7 1 1

7 1 3

7 1 4

7 1 5

7 1 6

IU ELECT & MECH MEASUREMENTS PART II

CALL No.

1 9 6

1 9 8

1 9 9

2 0 1

2 0 2

203

204

205

GUIDANCE & ST-124 MEASUREMENTS

IU MECh JYSTEMS PART I

IU VOLT/CURRENT MEASUREMENTS

GYRO-STAB

AUX POWER MONITOR

I

::: 1 2C6

FCC INPUT/OUTPUT PARAMETERS

CSP INPUT/OUTPUT PARAMETERS

I !

8 3 3

8 3 4

8 3 5

8 3 6

8 3 7

8 3 8

8 3 9

FLIGHT CONTROL END/END DIM

I

3 2 1

3 2 2

3 2 3

3 2 4

3 2 5

3 2 6

3 2 7

S-IC DISPLAY DESCRIPTIONS

GROUND HYDRAULIC mrr MONITOR

ENGINE HEATER MONITOR

S-IC PNEUMATIC SUPPLY MONITOR

S-l l LH2 PRECONDITIONING TEMPS

S-IC EMERGENCY TEMP MONITOR

S-IC STAGE BUS MONITOR

S-IC ESE BUS MONITOR

AUTMORIZED FOR VEHICLE

Page 57: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

Page 58: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn \/ Display Descriptions (Continued)

Page 59: JOHN F. KENNEDY SPACE CENTER

Table 1-9. Saturn V Display Descriptions (Continued)

DISPLAY DL%. NO.

943

944

945

946

947

948

949

950

K S C C O * U I I . I I "

1-5 2

CALL r(O.

431

432

433

434

435

436

437

438

I I C Y 08.1

DESCRIPTION

MEASURING - EMERGENCY TEMPS

MEASURING - DYNAMIC MEAR

MEASURING - ENGINE TEMPS

MEASURING - ENGINE PRESS

MEASURING - PRESS, HYDRAULICS

MECHANICAL - PRESS, LOX/FUEL

MECHANICAL - HYDRAULIC SYSTEMS

MECHANICAL - TEMPS, LOX PUMPS

REMARKS

FOR

N rc In

AUTHO RI VEHICLE

LCD

m a rcoa VIN3

X

X

X

X

X

X

X

X

Page 60: JOHN F. KENNEDY SPACE CENTER

Table 1-10. Saturn V Permanently Masked MDls

IODC Number Word Number MDI Numbers

7 32 2256 thru 2279

7 33 2280 thru 2303

2376 thru 2399

2400 thru 2423

2424 thru 2447

2448 thru 2471

2472 thru 2495

42 2496 thru 2519

58 2880 thru 2903

59 2904 thru 2927

60 2928 thru 2951

7 61 2952 thru 2975

7 ,' 62 2976 thru 2999 '

7 63 3000 thru 3024

NOTE - The L.DOs associated with the above MDls are updated every 12 seconds.

Page 61: JOHN F. KENNEDY SPACE CENTER
Page 62: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-12

. A

TO

LL

Sub

Pro

gram

s

1 N

AS

A A

UT

H.

I.

. I

EL

EM

EN

T A

ND

R

E SP

OW

SIBL

E C

ON

TR

AC

TO

R

PR

OG

RA

M T

ITLE

6 F

UN

CT

ION

FCC

S/C

IN

PU

T T

ES

T;

Uti

lizes

the

CC

lS te

st i

nput

s to

ver

ify t

he f

light

con

trol

co

mpu

ter

dc a

mpl

ifier

gai

n ch

ange

s fr

om 3

.75

to

10

.0 w

hen

S/C

co

ntro

l m

ode

is

i KZA

T

KZ

IT/

GD

C-2

IU

INT

ER

FA

CE

TE

ST

; S

ets

up p

rede

term

ined

bit

pat

tern

s in

the

addr

ess

regi

ster

I LZI

T

/ BATC

1 and c

heck

s re

spon

ses

via

the

veri

fy r

egis

ter

(oth

er i

ndic

atio

n).

LZ

TU

G

DC

4

S-I

B T

AR

GE

T U

PD

AT

E S

UB

RO

UTI

NE

; P

rovi

des

optio

ns f

or t

arge

t up

date

I l BAT

C

I para

met

ers

to b

e en

tere

d in

to L

VD

C.

IBM

I OZIT

lYt;: i S-IB

INT

ER

FA

CE

TE

ST

; S

et u

p pr

edet

erm

ined

bit

pat

tern

s in

the

addr

ess

regi

ster

an

d ch

ecks

res

pons

es v

ia th

e ve

rify

reg

iste

r.

OZ

PT

G

DC

-22

S-I

B P

OW

ER

TR

AN

SF

ER

; T

rans

fer

S-I

B S

tage

Pow

er ,m

tf vc

rifie

s re

sults

.

I ICC

SD I

2

SW

ITC

H T

ES

T;

Tes

t th

e st

art

and

rese

t sw

itche

s on

the

ED

S p

rep

pane

l, th

at

adva

nce

or r

ecyc

le th

e pr

ogra

m.

I

OZ

PV

G

DC

-24

PR

E-V

ALV

E T

IMIN

G;

Che

cks

SIB

pre

-val

ve o

peni

ny a

nd c

losi

ng p

er S

pec.

and

I

( CCS

D

crite

ria.

4r

u

zo

o

4a

v

OZ

EC

OZ

TV

OZ

FS

I GD

C-3

3

GD

C-2

2 C

CS

D

GD

C-3

3 C

CS

D

S-I

B F

LIG

HT

SE

QU

EN

CE

; V

erifi

er a

ll S

IB S

tsyc

Fliy

llt

Seq

uenc

e fu

nctio

ns.

w

i I ul

i V

,

S-I

C

ES

E C

UT

OF

F;

Che

cks

SIB

ES

E c

utof

f ci

rcui

t an

d pe

rforr

ns R

edun

danc

y T

est

S-I

B T

OP

S V

OTI

NG

; V

erify

2 o

ut o

f 3 v

otirl

y in

Thr

ust Low C

utof

f C

ircu

its.

I , CCSD

I X

x I I X I

Main Progra

m Q

AE

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ST

AT

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AN

D/O

R

RE

MA

RK

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Ma

in P

rogr

am V

AF

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in P

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S

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in P

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AL

L

Ma

in P

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AS

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KS

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OR

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6.22

6 (R

EV

. 5

69

) I

QZ

EC

AU

TH

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OR

V

EH

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! N

O.

g ,","

w

X

X X X I

X X X

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3

K

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aS

o

X X

X X X

TE

RF

AC

E

i w

Ma

in P

rogr

am O

AR

l

X X X X

GD

C-2

6 S

-ll

EN

G C

IRC

UIT

; P

erfo

rms

seco

nd p

art

of

Eny

inc

Con

trol

Tcs

t.s,

Spa

rk S

yste

m

I A

(C

ompo

nent

Tes

t.

and

Eny

inr

Sta

rt I

cqu

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ito

fl tc

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in P

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am O

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1

X I X

X

X X

X X X X X X

X X X X X X X

Page 63: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-1 2.

A

TO

LL

Sub

Pro

gram

s (C

ontin

ued)

QZ

EF

QZ

FC

QZ

IT

42

02

QZ

Tl

QZ

T2

vz3

3,

12

33

VZ

DS

, IZ

DS

n€R

m

NA

SA

*u

rn.

EL

EM

EN

TA

ND

R

ES

PO

NS

IBL

E

CO

NT

RA

CT

OR

GD

C-2

6 N

AR

GD

C-2

6 N

AR

GD

C-2

B

AT

C

GD

C-2

6 N

A R

INS

-21

N

AR

INS

-21

N

AR

GD

C-2

5 IB

M

GD

C-2

B

AT

C

,-a1

(RE

V.

149

PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

lil

I

S-l

l E

NG

CIR

CU

IT;

Per

form

s th

ird

part

of

eny

cont

rol

test

s.

Ill

S-l

l IN

TE

RF

AC

E T

ES

T;

Set

ps u

p pr

edet

erm

ined

bit

pat

tern

s in

the

addr

ess

regi

ster

an

d ch

ecks

res

pons

es v

ia t

he v

erify

reg

iste

r (o

ther

ind

icat

ion)

.

S-l

l S

WIT

CH

SE

L F

UN

CT

ION

; Is

sues

and

ver

ifies

pro

per

resp

onse

s to

the

follo

win

g:

S-l

l S

witc

h S

elec

tor

Com

man

ds:

Cha

rinel

s 7

, 12

, 1

4, 19, 20,

32

, 3

8,4

8,4

9,

56

, 58,

59

, 6

0,

61,

88

, an

d 9

9.

S-l

l C

OM

PL

DIS

CR

ET

E;

Ver

ifies

tha

t 11 2

disc

rete

mea

sure

men

ts (

56

Pai

rs)

are

in a

com

plem

enta

ry s

tate

. E

rror

s de

tect

ed i

ndic

ate

failu

re o

f a

digi

tal

subm

ultip

lexe

r,

DD

AS

ass

embl

y,

or d

iscr

ete

mea

sure

men

t su

bsys

tem

.

S-l

l D

ISC

RE

TE

ST

AB

LIZ

ER

; P

rovi

des

a di

agno

stic

rou

tine

to d

etec

t an

d as

sist

.i

n is

olat

ing

any

inst

abili

ties

whi

ch m

ay o

ccur

in

the

two

rem

ote

digi

tal

s~~

bmul

tipl

exer

s or

in

the

PC

M D

DA

S a

ssem

bly.

LVD

A/D

C 0.

0.

TE

ST

; C

heck

s th

e LV

DA

dis

cret

e ou

tput

s.

D&

tu

rns

on th

e L

V

GU

lD l

ight

ir!

the

S/C

. D

O6

turn

s on

the

LV

RA

TE

lig

ht i

n th

e S

/C w

hen

rate

abo

rt

is e

nabl

ed.

DO

12

che

cks

the

Fir

ing

Com

mit

enab

le i

nter

lock

in

the

IU re

ady

for

laun

ch c

hain

. 0013 c

heck

s th

e F

irin

g C

omm

it in

hibi

t in

the

IU ,

-Iv

for

lau

nch

chai

n.

DU

AL

SE

LE

CT

TE

ST

; ,s

sues

rea

d co

mm

ands

to

pro

vide

a r

egis

ter

test

out

put,

and

to v

erify

ES

E in

hibi

ts.

Page 64: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-12

. A

TO

LL

Sub

Pro

gram

s (C

ontin

ued)

AU

TH

. F

OR

NO

.

-.

~

5121

5

13

3.

06

t hru

2

09

V

20

6

th

~

209 1

ST

AT

US

AN

D,O

A R

EM

AR

KS

Mai

n P

rogr

am V

AE

D/

IAE

D

Mai

nPro

gram

VA

ED

/ IA

ED

Ma

inP

rog

ram

VA

SY

IA

SS

Mai

n P

rogr

am V

AT

S

Ma

in P

rogr

am V

AE

D

IAE

D

Ma

in P

rogr

am V

AE

D/

l AE

D

Mai

n P

rogr

am V

AE

W

IAE

D

w

S

PR

OG

RA

M T

ITL

E L

FU

NC

TtO

N

EN

GIN

E O

UT

AB

OR

T T

ES

T;

Ver

ifie

s th

e en

gine

thr

ust

circ

uitr

y an

d as

soci

ated

en-

ab

le a

nd a

bort

cir

cuit

ry b

y si

mul

atin

g ttc

e en

gine

thr

usts

wit

h tli

scre

tes

issu

ed b

y th

e co

mpu

ter.

Per

mut

ates

thr

ust

sign

als

to s

imul

ate

one

and

two

engi

nes

out,

atid

to

veri

fy th

e as

soci

ated

vot

ing

circ

uitr

y.

Sim

ulat

es th

e th

rust

sen

sors

of

theS

-Il

and

S-I

VB

eng

ines

.

The

pro

gram

pro

vide

s a

seco

nd fe

atur

e;

if F

lag

17

is s

et,

it s

elec

ts t

he $

PR

3,

5,

or 6

O

ptio

n in

VA

ED

; a

ll p

rogr

am s

tops

are

byp

asse

d.

EN

GIN

E C

UT

OF

F T

ES

T;

Is ru

n du

ring

wet

por

tion

of C

DD

T.

Che

cks

out

the

Ran

ge

Saf

ety

C/O

to

the

S-IC

and

S-l

l st

ages

and

ED

S o

utpu

t to

the

S-IC

, S

-ll,

and

S-I

VB

. T

he E

DS

cut

off

is a

ccom

plis

hed

by c

yclin

g th

e 6

D9

1,

60

92

, an

d 6

09

3 b

uses

on

and

off

in p

airs

. C

/O A

is

obt

aine

d by

tur

ning

off

the

6D

92

and

6D

93

bus

es.

C/O

B

is o

btai

ned

by tu

rnin

g of

f th

e 6

D9

1 a

nd 6

D9

3 b

uses

.

A F

LOA

TIN

G "

ON

ES

" T

ES

T;

Fun

ctio

nal

chec

k of

sw

itch

sele

ctor

.

VA

TS

TE

RM

GE

OL/

FE

50;

Use

d to

term

inat

e th

ese

two

func

tion

exec

utor

s at

an

appr

opria

te t

ime

in th

e ru

nnin

g of

VA

TS

(con

lput

er i

nter

nal

oper

atio

n).

VA

ED

ML

SR

LO

AD

;

RA

TE

EX

CE

SS

IVE

AB

OR

T T

ES

T;

Che

cks

the

YA

W,

PIT

CH

, an

d R

OL

L E

xces

sive

R

ates

, th

e E

nabl

e,

and

Dis

able

s, a

nd t

he a

ssoc

iate

d E

xces

sive

Rat

es A

UT

O-A

BO

RT

V

otin

cj L

ogic

.

1 S

PA

CE

VE

HIC

LE A

BO

RT

TE

ST

; C

heck

out

of t

he a

utom

atic

and

n~a

nual

sequ

ence

an

d co

ntro

l of

the

Lfi

and

S/C

Abo

rt S

yste

ms

unde

r si

mul

atec

! enl

erge

ncy

cond

ition

s.

Dur

ing

this

tes

t, a

ll m

anua

l ab

ort

inhi

bits

and

Ena

ble

circ

uitr

y is

ver

ified

alo

ng w

ith

S/C

cut

offs

to

the

vehi

cle.

- -

-~

lYA

R

vZ

EA

I lZ

EA

VZ

EC

I IZ

EC

VZ

Fl/

lZ

Fl

VZ

GT

VZ

ML

VZ

RE

/ IZ

RE

VZ

SA

/ iZ

SP

4-

OR

M

NA

SA

AU

TH

. E

LE

ME

NT

AN

0

RE

SP

OW

SIS

LE

CO

NT

RA

CT

OR

GD

C-2

5 IB

M

GD

C-2

5 IS

M

GD

C-2

B

AT

C

CA

P-A

B

AT

C

GD

C-2

5 IS

M

GD

C-2

5 IB

M

GD

C-2

5 1B

M

16.2

26 (

RE

V.

5,6

9)

K

2

en

::

W

X X X X X

F! - 0

o

A

z

>

m

0 X X

INT

ER

FA

CE

od

0 I

w

44

g2

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ou

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oo

o

X X

I I i X X X

!'

X X X X X X X

X X X X

I X X X

X

X X X

X

X X X

X X I X

Page 65: JOHN F. KENNEDY SPACE CENTER

Tab

le 1

-12

. A

TO

LL

Sub

Pro

gram

s (C

ontin

ued)

VZ

TT

1 C::;';",

VZ

TS

G D

C -2

4 W

ZCR

1 B

AT

C

CA

P-A

B

AT

C

WZ

Fi

I Gpti

33

WZ

IT

I Gii;:

GD

C-2

4 W

zpo

1 BA

TC

GD

C-2

4 W

ZRB

I B

AT

C

GD

C-2

2 W

ZS

P I B

AT

C

GD

C-2

3 X

ZCM

I M

DA

C

GD

C -2

3

XZ

DM

I M

DA

C

~R

M

16.2

26 (

RE

V.

5 6

9

I IN

TE

RF

AC

E

follo

win

g ex

ecut

ion

of e

ach

appr

cpri

ate

mac

hine

lan

guag

e te

st p

rogr

am ic

ornp

uter

int

erna

l op

erat

ion)

.

PR

OG

RA

M T

ITL

E 6

FU

NC

TIO

N

VA

TS

VM

TS

LO

AD

; Lo

ads

mac

hine

lan

guag

e su

brou

tine

VM

TS

as

rew

ire

d i

n V

AT

S

SE

GM

EN

T 1

OF

VA

TS

; S

ets

flags

to

indi

cate

sw

itch

sca

n fa

ilure

s an

d pe

rfor

ms

othe

r V

AT

S fu

nctio

ns f

rom

VA

TS

sta

rt t

o T

-18

min

utes

.

SE

GM

EN

T 2

OF

VA

TS

; S

ame

func

tion

as s

egm

ent 1 fro

m a

ppro

xim

atel

y T

-16

:30

to

T

-10

:30

. I lX

/X~XIX

IX/XIX

P v

0

>

CU

TO

FF

RE

LA

YS

RE

DU

ND

AN

T B

US

TE

ST

; Is

olat

es r

edun

dant

bus

es a

nd v

erifi

es

indi

vidu

al b

us c

apab

ility

to

give

cut

off.

SW

ING

AR

M P

OW

ER

UP;

F

irin

g po

wer

43

D1

00

and

43

02

00

. I

i

",

CU

TO

FF

RE

LA

YS

FU

NC

TIO

NA

L;

Sho

rt f

unct

iona

l te

st o

f cu

toff

cir

cuit

ry u

sed

to v

erify

ci

rcui

try

prio

r to

eac

h in

divi

dual

inte

grat

ed t

est.

EB

W C

HA

RG

E F

IRE

; T

ests

for

ret

ro a

nd s

epar

atio

n E

BW

firi

ng u

nit c

harg

ing

and

firin

g un

der

prop

er a

nd im

prop

er c

ondi

tions

.

S4

VB

DD

AS

AU

TO

MA

TIC

SC

AN

I lXl lX

l lXIX

Xi I lX

XIX

I Ix

I

:

S-I

VB

D

DA

S A

UT

OP

IAT

IC S

CA

N

I lXl

IXI lX

IX

CC

U3

3Z

zoo----

S-I

C

EN

G N

OT

ZE

RO

TE

ST

; T

oq

ue

s th

e E

DS

/CR

G

to a

scer

tain

the

S-I

C e

nqrn

e (n

ot -

zero

) in

dica

tion

set

leve

ls.

1 IXi ix

S-I

C

INT

ER

FA

CE

TE

ST

; S

ets

up p

rede

term

ined

bit

pat

tern

s in

the

ac!c

!ress

rey

iste

r an

d ch

ecks

res

pons

es v

ia t

he v

erify

reg

iste

r (o

ther

ind

icat

ion)

. X

1'

i 1

,

I /

SW

ITC

H S

CA

N;

Sca

ns S

-IC

pa

nels

for

pro

per

switc

h po

sitio

ns.

S JV

B

DD

AS

AU

TO

MA

TIC

SC

AN

ST

AT

US

AN

D:

OR

RE

MA

RK

S

Mai

n P

rogr

am V

AT

S

Mai

n P

rogr

am V

AT

S

2~

zz

cc

t

ou

~~

oa

v

Mai

n P

rogr

am W

AC

R

Mai

n P

rogr

am W

AS

V

Ma

in P

rogr

am V

AF

C

Mai

n P

rogr

am V

AS

S

-I

Mai

n P

rogr

am W

AP

O

Mai

n P

rogr

am W

AC

R

=>

::

-

AU

TH

. F

OR

V

EN

lCL

E

NO

. -

51

2/

51

3

51

2/

513

5i2

/ 5

13

51

2/

51

3

51

2/

51

3

51

2/

51

3

51

2/

,51

3

51

2/

51

3

I 51

2

51

2

51

2

-

7

a%

%

X X

Mai

n P

rogr

am X

AD

A

Mai

n P

rogr

am X

AD

A

X

Ma

in P

rogr

amX

AD

A

Page 66: JOHN F. KENNEDY SPACE CENTER

xz lC

/ E

ZlC

XZ

IT/

EZ

lT

XZ

MN

XZ

PD

XZ

PU

3c F

OR

M 5

Tab

le 1

-1 2.

A

TO

LL

Sub

Pro

gram

s (C

ontin

ued)

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

GD

C-2

S

-IV

B I

NT

ER

FA

CE

TE

ST;

S

ets

up p

rede

term

ined

bit

pat

tern

s in

the

addr

ess

regi

ster

B

AT

C

and

chec

ks r

espo

nses

via

the

veri

fy r

egis

ter

(oth

er i

ndic

atio

n).

1

PR

OG

RA

M T

ITL

E 6 F

UN

CT

ION

GD

C-2

3 M

DA

C

GD

C-2

3 S

-IV

B D

DA

S A

UT

OM

AT

IC S

CA

N

MD

AC

1 S

-IV

B

INIT

IAL

CO

ND

ITIO

N S

CA

N

G DC

-23

M D

AC

S

-IV

B P

OW

ER

DIS

TR

IBU

TIO

N;

Ver

ifies

pcw

er d

istr

ibut

ion

atid

con

trol

sw

itchi

ng

circ

uits

.

? - 0

S S

T A

TU

S A

ND

/OR

R

EM

AR

KS

E :

+ -

Ma

in P

rogr

am X

AIC

/ E

AlC

i i I "

44

Uf

Z

OO

"

4o

ul

X

X

X

X

-

5 2 Z

&&

-

aZ

x

00

0

XX

K

XX

X

XX

X

XX

X

XX

K

Ma

in P

rogr

am V

AS

S/

IAS

S

Ma

in P

rogr

am X

AD

A

I M

ain

Pro

gram

XA

PD

INT

E

0

O I

a

W 1

1

Ma

in P

rogr

am X

AP

D

(for

51

2)

Ma

in P

ro-

gram

XA

PU

(fo

r 5

12

)

-

AU

TH

. F

OR

V

EH

ICL

E

NO

.

-

51

2/

20

6

thru

2 09

J. 51

2

5 1

2

51

2

-

Page 67: JOHN F. KENNEDY SPACE CENTER

SECTION II OFF-LINE PROGRAMS

2 - 1 GENERAL

This section l is ts a l l the off-line programs for the Saturn It3 and Saturn V launch vehicle operations. Information contained i n the tabular portion includes IVARS, Program Tit les and Function Descriptions, Listing and Document Revision levels, andRelease Dates (or change document status for unreleased prog- rams). The following tables appear i n this section:

a. Table 2- 1, RCA- 11 OA Supplemental Diagnostic Programs; These programs are used for preventative maintenance and problem isolation within the RCA-1 1OA and i ts peripheral equipment.

b. Table 2-2, RCA-11OA Supplemental Ut i l i ty Programs; These programs perform functions common to a l l applications.

c. Table 2-3, RCA-11 OA Supplemental Postprocessing Programs; These programs are used for retrieving discrete and non-discrete data logged on the Saturn System Log tapes.

d. Table 2-4, DDP-224 Suppleniental Programs; These programs are used for DDP-224 maintenance an(' 9DP-224 /RCA- l lOA interface.

e. Table 2-5, DEE-6CE Supplemental Diagnostic Programs; These programs are used for preventative maintenance and problem isolation on the DEE-(ICE (SDS 9 3 0 / 0 9 2 ) computers.

f. Table 2-6, DEE-6C/E Supplemental Ut i l i ty atid Postorocesslnq Proc~ra~ns; These programs are used to reduce the datd recorded by tlle DEE-6C/E scan programs.

2-2 KSC FORM 16-226A

A l l programs listed in paragraph 2 - 1 use the same KSC form to presetit the ass~ciated information for each program. An explanation of the siqnificance of headings and columti t it les, arid guideii~ies for interpreting the tables 3re as follows:

a. IVAR; The Internal Variable l istit ig i n alpl~anumer~cal seqrlericc (programs not assiyned an IVAR w i l I appear at the end of the table as N/A).

b. NASA Auth Element and Responsible Contractor; The mai I code syrnbo: (must be preceded by LV) of the NASA agency, and tho mriemonic name of t:,e responsible contractor.

c. Program Tit le and Function; The t i t le of the program and a short description of its function.

d. Rev.; The LISTING and/or the DOCUMENT columns indicate the latest revision level for both l i s t i ~ s and documents.

e. Last Release Date; Indicates the date of the latest rev ision of the prograrii.

f. Unreleased Program Status, or Open Change Documents (CPCR-PTR); Ustd to indicate an unreleased program, program being released, or generhl remarks, as required.

Page 68: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-1.

RC

A-1

1 O

A S

uppl

emen

tal

Dia

gnos

tic P

rosr

ams

IVA

R

AJT

CP

Ul

CP

U2

CP

U3

NA

SA

AU

TN

. E

LE

YE

NT

AW

O

RE

SP

ON

SIB

LE

C

ON

TR

AC

TO

R

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IS

M

GD

C-3

1

PR

OC

RA

M T

ITL

E A

ND

FU

NC

TIO

N

I IB

M

DE

MP

G

DC

-31

I 'B

M

GD

C-3

1

I IB

M

DIC

P

DL

11

DL

lS

DO

IT

DR

UM

DS

06

I G

DC

-31

IBM

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

IB

M

GD

C-3

1 IB

M

GD

C-3

1

IBM

UN

RE

LE

AS

ED

PR

OC

RA

U

ST

AT

US

. O

R O

PE

N

CH

AN

GE

D

OC

Uu

EW

TS

10

-28

-69

6-9

-69

05

/12

/72

RE

V. t Z

IcP

CR

-PT

R)

LA

ST

R

EL

EA

SE

A

I 0 3

I I

DIS

CR

ET

E E

VE

NT

S M

ON

ITO

R;

Ver

ifies

the

pro

per

aper

atto

n of

the

ML

RC

A-1

1OA

co~

nput

er/L

L'G

C

1 1

DA

TE

02

/25

/71

10

-01

-68

3-1

1-6

9

3-1

1-6

9

inte

rfac

e un

it p

rior

to

LVD

C ~

nsta

llati

on.

DA

ILY

DIS

CR

ET

E T

ES

T;

Ver

ifies

the

pro

per

opera

tion o

f th

e di

scre

te o

utpu

t ci

rcu

~tr

y aiid

the

Dis

cret

e C

ontr

ol E

quip

men

t.

RC

A-1

1OA

/DD

P

22

4 I

NT

ER

FA

CE

:11

OA

SID

E);

Che

cks

the

IOD

C-6

/DE

CV

fo

r se

nse

bit

pat

ters

and

bl

ock

data

tra

nsfe

r.

2A

2A

Non

e

1

i 4E

t: 0 1 C

C

C

I 2 0

13

DA

TA

1 IN

K I

NT

ER

FA

CE

; T

ests

dat

a lin

k !)e

twee

li B

H'L

CC

an

d A

GC

S./M

L R

CA

-11O

A C

ompu

ters

(d

iagn

ostic

).

5-13-70

/

ALA

RM

JU

MP

TE

ST;

C

heck

s th

e op

era!

ion

of t

he R

CA

-11O

A j

ump

c~rc

uit

ry.

CE

NT

RA

L P

RO

CE

SS

OR

1;

Che

cks

oper

atio

n of

the

RC

A-1

1OA

in

stru

ctio

n re

pert

oire

and

ind

icat

es a

ny

failu

res

incu

rred

, al

ong

wit

h a

poss

ible

cau

se o

f fa

~lu

re.

CE

NT

RA

L P

RO

CE

SS

OR

2;

Com

plet

es v

erifi

catio

n of

the

RC

A-1

1OA

~rr

stru

ctio

ri re

pert

owe

arid

aug

men

ts

cent

ral p

roce

ssor

dia

gnos

tic (

Tes

t A

).

BA

NK

2 O

F C

PU

2;

2

5-1

3-7

0

N/A

1-0

4-6

9

12/3

3'70

5 J I 0 8 8

Inte

rrel

ated

w/D

LI

BA

NK

2 O

F D

LIT;

I 3

DIS

CR

ET

E O

UT

PU

T/IN

PU

T;

Tes

ts t

hc D

CE

in

Cab

inet

8 b

y is

suin

g o

ff-l

1r2

DO

s pl

ugge

d to

the

IOD

Cs;

in

duce

s M

TO

AD

and

-.x

clus

~vi

ty fa

ilure

che

cks

the

DC

E r

espo

nse.

DR

UM

AN

ALO

G;

Writ

es a

nd r

eads

cyc

ling

drum

pat

tern

s fo

r sc

op;n

y sr

ynal

s.

0 1

DIS

CR

ET

E I

NP

UT

MO

NIT

OR

; V

erifi

es d

iscr

ete

inte

rfac

e by

log

ging

and

com

parin

g ln

oni

led

dis

cret

es-in

.'

I

Page 69: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-1.

RC

A l

lOA

Sup

plem

enta

l D

iagr

bost

ic P

rogr

ams

(Cor

rtinu

ed)

-..

--

-- -

-- ---

-

-4

NA

SA

AJ

TH

. E

LE

ME

NT

AN

D

PR

OG

RA

M T

ITL

E A

ND

FU

NC

TIO

N

05

36

L

DS

ll

DS

14

- z A 5 1

2 3

B

B

0 4

i A

RE

V. I-

5 2 :: 0 4E

A

P F

3-2

1-6

9

, -1

-11

-69

7-2

4-6

8

10

-01

-68

2-2

8-6

9 I

CG

WT

RA

CT

OR

GD

C-3

1 IB

M

GD

C -

31

IS

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

- ,

D

I

- -

----

I L

AS

i R

EL

EA

SE

D

AT

E

12

/03

/7C

12

-10

-68

12

-10

-68

2-2

2-7

2

2-2

2-7

2

4-6

-72

TA

F2

CS

17

--

PA

RT

It

OF

05

06

:

RE

MO

TE

ME

MO

RY

DIA

GN

OS

TIC

, P

rovi

des

diag

nost

c ,

*lclly

: is

of

ttlc

RC

A-1

10

A h

igh-

spee

d m

emor

y fo

r th

e un

man

ned

ML

. (P

rcgr

am I

S d

esig

ned

for

slow

,ys

tem

re

cove

ry.)

RE

MO

TE

PR

KE

SS

OR

, T

ES

T A

; C

heck

s op

erat

~on

of 2

7 M

LC

or

AG

CS

C R

CA

-1lO

A o

~e

rati

on

code

s,

indi

catin

g al

ly f

ailu

res

incu

rred

, al

ong

wit

h a

po

ss~

hle

caus

e of

fai

lure

. (P

royr

am i

s de

siyn

ec f

or s

low

sy

stem

rec

over

y .)

TA

PE

SY

ST

EW

DlA

Ghr

OS

TIC

TID

ES

II, P

AR

T I; P

erf

ar~

l~sZ

O

star

t-sr

yial

l, lo

gic

and

mec

l~ar

iical

test

s on

sel

ecte

d M

TS

to is

olat

e fa

~lu

res.

h) 1

W

UN

RE

LE

AS

ED

PR

OG

RW

S

TA

TU

S.

OR

OP

EN

C

HA

NG

E D

OC

UY

EN

TS

(C

PC

R-P

7R

)

Inte

rrel

ated

w/D

S0

6

Inte

rrel

ated

w/,/

DS

ld

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IQ

M

GD

C-3

1 lB

M

GD

C-3

1 IB

M

16.2

164

45

69

,

DS

19

I D

SZ

l

05

23

DS

2A

GS

25

KS

C F

OR

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

RE

MO

TE

DR

UM

DIA

GN

OS

TIC

; T

e-tq

the

a!>

il~ty

to r

ead

and

wr~

te 01

1 th

e u1

1-an

ned

ML

~r

AG

CS

R

CA

-11

OA

dru

m w

ithou

t pa

rlty

err

or.

fPro

grar

n IS

de

sr~

ne

d for

slo:v

syst

elv

r. , o

vrry

.)

RE

GlS

TE

PR

OC

ES

SO

R,

TE

ST

E;

Che

cks

oper

atio

n of

45

ML

C o

r A

GC

SC

RC

A-1

1OA

ope

rztio

n co

des,

in

dica

ting

any

failu

res

~ncu

rred

, alo

riq w

it11

a p

oss

~b

le ca

use

of f

ailu

re.

!Pro

yam

IS

desc

gned

for

slo

w

syst

em r

ecov

ery.

IOD

C C

OM

PA

TIB

ILIT

Y T

ES

T;

E?c

ures

pro

per

opcr

atio

ri !)e

twee

ri IO

DC

5 ar

id a

ssoc

iate

d ~n

put/

outp

ut

devi

ces.

AN

ALO

G S

YS

TE:v

l C

ALI

BR

AT

ION

; C

al~

brat

ez ar

lala

y s\

ster

n us

ing

~n

pu

t corlt

rol d

ata

via

sells

e sw

itcir

cont

rol.

MA

GN

ET

IC T

AP

E A

K4L

OG

CH

EC

KO

UT;

Cfie

cks

the

rna

qrie

t~c t

ape

aria

loy

c~

rcu

~ts

by

rea

ding

a~

ld

wri

ting

diff

eren

t lie

y t >

~r

? pa

tterir

s.

A 2

0 A

1

TA

PE

SY

ST

EM

DIA

GN

OS

TIC

TA

PE

S II, P

AR

T II;

I / DR

!.i;A D

IAG

NO

STI

C;

Test

s ab

ility

to

rear

! ,~

rlr!

wrr

t- 0

11 tI,

e R

CA

-11O

A

dr~

rn~

w

ithou

t pa

rity

err

or.

8

Page 70: JOHN F. KENNEDY SPACE CENTER

! f f , L KSC FORM 14

N .&

NA

SA

AU

TH

. E

LEM

EN

T A

ND

R

ES

PO

NS

IBLE

C

ON

TR

AC

TO

R

WA

R

DS

26

DS

P6

OS

28

DP

28

DS

38

ME

Ml

SC

P

3v

r~?

NT

ST

INS

-13

IBM

INS

-13

IB

M

GD

C-3

1 IS

M

GD

C-3

1 IB

M

GD

C-3

1 IS

M

GD

C-3

1 IB

M

f26

A (

S/6

9)

Tab

le 2-1.

RC

A-

.10

A S

uppl

emen

tal

Dia

gnos

tic P

rogr

ams

(Con

tinue

d)

PR

OG

RA

M T

ITL

E A

ND

FU

NC

TIO

N

10

z

I s

I

DD

AS

IN

TE

RF

AC

E A

CC

EP

TA

NC

E;

Fun

ctio

nally

che

cks

the

oper

atio

n of

the

DD

AS

CIT

-11

sys

tem

. 2

I ' SE

CO

ND

BA

NK

OF

DS

26;

3

CLO

CK

OV

ER

ALL

TE

ST

; C

ombi

nes

the

3-P

IT,

RTC

, C

OC

, an

d C

MT

~~i

airll

ell,l

ice

test

s in

to o

ne

cc ~

cvli

da

ted

time

tes

t.

CI

I

.. .

. F .)G

RA

M F

OR

DS

28;

IOR

AN

D T

PC

TE

ST;

P

erfo

rms

pred

efin

ed te

sts

of T

PC

reg

iste

r to

insu

re i

t is

ope

ratio

nal

prio

r to

veh

icle

sup

port.

ME

MO

RY

DIA

GN

OS

TIC

; P

rovi

des

d~ag

nost

ic an

alys

is o

f th

f. R

CA

-11O

A h

igh

spee

d nl

erno

ry.

SE

NS

E C

ON

TR

OL

PA

NE

L C

HEC

KOU

T; C

heck

s lo

r pa

rity,

ex

clus

ivit

y an

d M

TO

AD

err

ors.

DC

E S

EL

F T

ES

T;

DC

E S

ELF

TE

ST

TA

BLE

S;

Tab

les

for

use

wit

h S

VD

P.

UN

RE

LE

AS

ED

PR

OG

RA

M

ST

AT

US

. O

R O

PE

N

Ri;{iE- 1 CHANGE DO

CU

ME

NT

S

1 a

(CP

CR

.PT

RI

U

Page 71: JOHN F. KENNEDY SPACE CENTER

lVA

R

FU

03

I

MS

FC

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

BO

OT

CD

AC

FU

07

I M

SF

C

CA

P-B

CA

P-B

I

(SC

FO

RM

16

-22

6A

0 6

9)

MU

03

TC

AC

Tab

le 2

-2.

RC

A-1

1OA

Sup

plem

enta

l U

tili

ty P

rogr

ams

CA

P-A

IB

M

CA

P-B

PR

OG

RA

M 1 IT

LE A

ND F

UN

CTI

ON

RE

V.

LA

ST

S

TA

TU

S,

OR

OP

EN

R

EL

EA

SE

I CH

AN

CE

DO

CU

ME

NT

S

(CP

CR

-PT

R)

I UW

RE

LEA

SE

O P

RO

GR

AM

CA

R[

DU

PE

AN

D/O

R

CO

MP

AR

E;

Dup

licat

es a

nd/o

r co

mpa

res

card

s,

list

s B

CD

car

ds,

and

dum

ps

bina

ry c

ards

. I

I I 7-

14-69~

7 A

CT

ION

TA

BL

E O

PE

RA

TIO

NA

L M

AIN

TE

NA

NC

E;

Gen

erat

es a

ctio

n ta

bles

and

lis

ting

s fo

r op

erat

ing

syst

em ta

pes

as r

equi

red

due

to a

ctio

n ta

ble

chan

ges.

UX

EX

BO

OT

ST

RA

P L

OA

DE

R;

Pri

nts

inst

ruct

ions

for

load

iny

UY

EX

the

n lo

ads

the

appr

opria

te r

outin

es.

LVD

C #

JON

-FLI

GH

T T

AP

E L

IST

/ED

IT,

BA

NK

1;

Pro

vide

s a

list

ful

lctio

n fo

r se

quen

ctng

and

an

edit

11

func

tion

for

upda

ting

the

varia

ble

tabl

es w

ithi

n th

e LV

DC

Veh

icle

Tes

t P

rogr

am (

VT

P).

1 5

E

0

DIS

PL

AY

DE

SC

RIP

TIO

N B

INA

RY

TA

PE

ME

RG

E;

Mer

ges

stag

e bi

nary

dis

play

des

crip

tion

tape

s in

to

a m

aste

r bi

nary

dis

play

des

crip

tion

tape

.

LVD

C N

GN

-FLI

GH

T

TA

PE

LIS

T/E

DIT

, B

AN

K 2

; P

rovi

des

a li

st fu

nctio

n fo

r se

quen

cing

and

an

edit

13

fu

nctio

n fo

r up

datin

g th

e va

riab

le ta

ble;

w

ithi

n th

e LV

DC

VT

P.

0

5F

4A

LVD

C N

ON

-FLI

GH

T T

AP

E L

IST

/ED

IT,

BA

NK

4;

Pro

vide

s a

list

func

tion

for

sequ

enci

ng a

nd a

n ed

it fu

nctio

n fo

r up

datin

g th

e va

riabl

e ta

bles

wit

hin

the

LVD

C V

TP

. I

10

-2-7

0

1-1

2-7

0

LVD

C N

ON

-FLI

GH

T T

AP

E L

IST

/ED

IT,

BA

NK

3;

Pro

vide

s a

list

func

tiori

for

sequ

enci

ny a

nd a

n ed

it fu

nctio

n fo

r up

datin

g th

e va

riabl

e ta

bles

wit

hin

the

LVD

C V

TP

.

LVD

C N

ON

-FLI

GH

T

TA

PE

LIS

T/E

DIT

, B

AN

K 5

; P

rovi

des

a l'i

st f

unct

ion

for

sequ

enci

ng a

nd a

n ed

it fu

nctio

n fo

r up

datin

g th

e va

riab

le ta

bles

wit

hln

the

LVD

C V

TP

.

10

LVD

C N

ON

-FLI

GH

T T

AP

E L

IST

/ED

IT,

BA

NK

6;

Pro

vide

s a

list

func

tion

for

sequ

enci

ng a

nd a

n ed

it

func

tion

for

upda

ting

the

varia

ble

tabl

es w

ithi

n th

e LV

DC

VT

P.

1 L/

V G

SE

VE

HIC

LE M

EA

SU

RE

ME

NT

CA

RD

VA

LID

AT

OR

; R

uns

a pr

eche

ck o

n a

ll m

easu

rem

ents

car

ds

I 1

prio

r to

:hei

r be

ing

rele

ased

, to

be

used

for

gene

ratin

g th

e m

easu

rem

ent

tabl

es.

I T

AP

E C

OP

Y A

ND

/OR

C

OM

PA

RE

; C

opie

s an

d/or

com

pare

s ca

rd d

ecks

or

tape

s ~n

BC

D o

r bi

nary

, pa

cked

I 0

or u

npac

ked,

wit

h an

y co

rnbi

natio

n of

inp

ut/o

utpu

t. I

Page 72: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-2.

RC

A-1

10-A

S

uppl

emen

tal

Uti

lity

Fro

gram

s (C

ontin

ued)

- -

-

NA

SA

NT

H.

EL

EM

EN

T A

ND

lV

AR

R

ES

PO

NS

lBL

E

I I C

ON

TR

AC

TO

R I

PRO

GR

AM

TIT

LE

AN

D F

UN

CT

ION

T L

ST

UP

20

UP

MP

CA

P-B

I U

TIL

ITY

TA

PE

DU

MP

; P

rint

s B

CD

fo&

atte

d ta

pes

or d

umps

tap

es o

f an

y fo

rmat

, na

mel

y bi

nary

or

sym

bolic

.

SA

TU

RN

V A

TO

LL

VA

LID

AT

OR

; T

ests

th?

abi

lity

of t

he A

TO

LL

pro

cess

or t

o de

tect

inv

alid

val

idat

or

IBM

C

AP

-B

I oper

ator

s.

I UPT

A

I I M

AG

TA

PE

VE

RIF

Y;

Ope

rate

s as

an

off-

line

uti

lity

pro

gram

to v

erify

tha

t th

e m

agne

tic ta

pes

to b

e us

ed

for

oper

atio

nal

supp

ort

logg

ing

are

of s

uch

qua1

ity

to g

ive

favo

rabl

e re

sult

s.

CA

P-B

CA

RD

IM

AG

E T

AP

E E

DIT

OR

/GE

NE

RA

TOR

; P

erfo

rms

all

pur

pose

:ar

d im

age

edits

, al

sc e

dits

DE

E-6

I I U

PTE

I

I poin

t qu

estio

n ta

bles

.

llO

A/D

EE

-6

TA

BL

ES

ME

RG

E P

RO

GR

AM

; M

erge

s D

EE

-6 O

PS

Sys

tem

PA

tab

les

wit

h D

EE

-6

Mon

arch

ID

tabl

es f

or i

nput

to

UP

26

.

I UV

SS

1 C

AP

%

I llO

A/D

EE

-6

UT

ILIT

Y P

AC

KA

GE

; C

ontr

ols

perip

hera

l eq

uipm

ent

for

off-

line

uti

lity

pro

gram

s.

UX

E D

UX

EX

UX

ML

YS

AC

Y S

AE

CA

P-B

CA

P-B

CA

P-B

CA

P-A

CA

P-A

11

0A

OF

F-L

INE

ED

ITO

R;

Edi

ts o

ff-l

ine

prog

ram

s be

ing

mai

ntai

ned

on t

he U

XE

X s

yste

m ta

pe a

s w

ell

as l

oadi

ng a

nd/o

r ex

ecut

ing

prog

rain

s th

at a

re i

n a

ssei

nble

r ob

ject

, ra

w b

inar

y fo

rin (

card

s or

tap

e),

or

DA

P b

inar

y de

cks,

to

be

adde

d to

the

syst

em ta

pe.

11

0-A

OF

F-L

INE

EX

EC

UT

IVE

; C

ontr

ols

the

load

ing

a*id

exe

cutin

g of

off

-lin

e pr

oyra

tns

unde

r it

s co

ntro

l.

11

0A

MIN

I LO

AD

ER

PR

OG

RA

M;

Pro

vide

s a

bina

ry c

ard

load

er c

apab

le o

f lo

adin

g S

LAP

, T

AM

E,

or

pure

bin

ary.

PR

EC

OM

PIL

AT

ION

AT

OL

L V

ALI

DA

TO

R;

Red

uces

pro

gram

che

ckou

t tim

e vi

a sc

rutin

izat

ion

of p

rogr

am

impu

lse

oper

ator

s pr

ior

to o

n-l

~n

e

chec

kout

. A

TO

LL

nR

AN

SL

AT

OR

SY

ST

EM

LO

AD

ER

YS

CP

YS

CT

CA

P-A

CA

P-A

ICD

TA

PE

CO

MP

AR

E A

ND

UP

DA

TE;

Con

sist

s of

5 s

ub-p

rogr

ams

com

bine

d to

form

1 pr

ogra

m.

They

ar

e th

e up

date

pro

gram

, Y

SC

P,

high

spe

ed l

ist,

LI

ST

, ca

rd li

sl,

CR

EA

D,

char

acte

r ti

tle

che

ck,

DE

EC

, an

d ta

pe c

ompa

re,

CO

MP

.

IVA

R C

AR

D T

ITLI

NG

; T

his

prog

ram

sea

rche

s th

e IC

D ta

pe a

nd p

rint

s th

e di

scre

te n

ames

for

the

AT

OM

IV

AR

cro

ss-r

efer

ence

ca

rds

supp

lied

as p

rogr

arr

:npu

t.

I

L I

WSC

FO

RM

1C

-226

A 1

5 69

1

UN

RE

CE

AS

ED

PR

OG

RA

M

ST

AT

US

, O

R O

PE

N

CH

AN

CE

D

OC

UM

EN

TS

(C

PC

R-P

TR

)

Lis

tin

g D

ate

1-1

1-7

1

LA

ST

R

EL

EA

SE

D

AT

E

1-1

9-7

1

2 2

RE

V. +

a ;

2

1-1

2-7

2

Pre

limin

ary I R

elea

se

3-8

-71

11

-18

-6

3-9

-72

4-1

-72

9-2

4-7

0

9-2

4-7

0

7-2

8-6

9

7-0

1-7

0

3-1

3-7

2

5-1

0-7

2

10

-02

-70

10

-02

-70

0 1

1A

2 26

5 10

2

0 0 0 3 0

3 ;

1

1A

2 0 5 5 2 4 2 2 3 3

Page 73: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-2.

RC

A-1

10-A

S

uppl

emen

tal

Uti

lity

Pro

gram

s (C

ontin

ued)

RE

V.

NA

SA

AU

TH

. E

LE

ME

NT

AN

D

CO

.(T

RA

CT

OR

PR

OG

RA

M T

ITL

E A

ND

FU

NC

TIO

N

AT

OM

ffS

CP

B

OO

TS

TR

AP

LO

AD

ER

; T

his

prog

ram

load

s Y

SL

2 v

ia th

e pr

eloa

d/lo

ad

swit

ch o

n th

e co

ntro

l pan

el.

AT

OM

ffS

CP

LO

AD

ER

AN

D C

ON

TRO

L;

Thi

s is

the

loa

der

and

cont

rol p

rogr

am fo

r Y

SC

P a

nd A

TO

M.

AT

OL

L T

O E

NG

LIS

H T

RA

NS

LAT

OR

SY

ST

EM

LO

AD

ER

AT

OL

L M

LS

R C

OM

PA

RE

PR

OG

RA

M;

Wil

l co

mpa

re t

he M

LS

R i

n th

e A

TO

LL

pro

yral

li to

the

rA

case

d ba

selin

e M

LS

R a

nd i

dent

ify d

iffer

ence

s,

if a

ny.

ME

SS

AG

E O

UT

PU

T/IO

DC

CO

NT

RO

L FO

R T

HE

YS

LT

SY

ST

EM

.

VE

RB

AG

ER

ET

RIE

VP

LF

OR

TH

EY

SL

T S

YS

TE

M.

LA

ST

R

ELE

AS

E

DA

TE

JNR

ELE

AS

ED

PR

OG

RA

M

ST

AT

US

, O

R O

PE

N

CH

AN

GE

DO

CU

ME

NT

S

(CP

CR

-PT

R)

Page 74: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-3.

RC

A-1

1OA

S

uppl

emen

tal

Pos

tpro

cess

ing

Pro

gram

s

*FU

DD

G

DC

-32

DD

AS

DIG

ITA

L T

AP

E G

EN

ER

ATO

R;

Rea

ds U

DA

S a

nd w

rite

s tli

e da

ta fr

om :h

e sp

ecia

l ad

dres

s on

a

I IBM

1 digi

tal t

ape

that

can

be

read

by

any

digi

tal

com

pute

r.

IVA

R

%U

NN

G

DC

-32

TM

DIG

ITA

L T

AP

E P

OS

TPR

OC

ES

SO

R;

Pro

vide

s t!i

e ca

pabi

lity

to r

ead

a di

gita

l ta

pe i

n th

e sp

ecifi

ed

I IBM

I fo

rmat

and

out

put

the

requ

este

d da

ta o

n th

e lin

e pr

inte

r.

TA

PE

CO

NV

ER

TER

; C

onve

rts

data

com

ing

from

a s

peci

fied

inpu

t ta

pe a

nd t

hen

writ

es t

he c

onve

rted

dat

a on

a s

econ

d ta

pe.

I

ID

DR

I CAP

-B

I OF

F-L

INE

D

l !',C

RE

TE

RE

TR;E

VA

L;

NA

SA

Alp

"'.

ELE

ME

I.

J

RE

SP

ON

SIB

LE

CO

NT

RA

CT

OR

VU

OO

zvo2

1

I OFF

-L.IN

E

QU

lCK

-LO

OK

D

ISC

RE

TE

DA

TA

RE

TR

IEV

AL;

Pro

vide

s a

Illca

ns o

f re

trie

ving

the

logg

ed

disc

rete

dat

a on

the

Sat

urn

V s

yste

m l

og ta

pe-

.

PRO

GR

AM

TIT

LE

AN

D F

UN

CT

ION

GD

C-3

2 IB

M

IV

AT

I CAP

-B

I AT

OL

L T

RA

CE

DA

TA

/FLI

GH

T

CO

MP

UT

ER

DA

TA

RE

TR

IEV

AL;

Ret

rieve

s da

ta l

ogr~

ed un

der

tlie

AT

CO

or

FL

Y 1 he

ader

s.

ZV

ET

( C

AP

-B

I EV

EN

TS

TR

AIl.

; P

rovi

des

a tim

e hi

stor

y o:

even

ts w

liich

occ

urre

d d!

lr~ng

a S

atur

n V

tes

t or

la

u~

~c

h.

ZV

MS

I C

AP

-B

I ZV

MT

SY

ST

EM

ME

SS

AG

E P

AC

KA

GE

;

lV

MT

I CAP

-B

I MT

Ol

TA

PE

PO

ST

PR

OC

ES

SO

R;

Pro

c,es

ses

each

DD

AS

sam

ple

loyy

ed b

y M

TO

l ar

id g

ives

the

ou

tput

in

vol

ts 0.

engi

neer

ing

units

.

SU

BP

I CA

P-B

I SU

BII

OU

TIN

E P

AC

KA

GE

FO

R Z

VR

E O

NLY

;

ZV

RE

I CA

P-B

I

NO

N-.D

ISC

RE

TE:

DA

TA

RE

TR

IEV

AL;

R

etrie

ves.

fo

rmat

s,

and

list

s se

lect

ed d

ata

from

the

SV

log

tape

r an

d ca

n pr

ovid

e nn

oct

al d

urt~

p of

the

log

tape

wit

h he

ader

inf

orm

atio

n de

code

d.

1,-

SC F

OR

M 1

6-21

6A (

5 69)

ZV

SS

UN

RE

LE

AS

ED

PR

OG

RA

M

LA

ST

S

TA

TU

S,

OR

OP

EN

R

EL

EA

SE

C

HA

NC

E D

OC

UM

EN

TS

D

AT

E

(CP

CR

-PT

R:

*MS

FC

G

el iv

ered

Pro

gram

CA

P-B

I/

O '

5UB

RO

UTI

FIE

PA

CK

AG

E;

Con

trol

s a

ll p

erip

liera

l eq

uium

ent

for

Sat

urn

V p

ostp

roce

ssic

q pr

ogra

n~s

Page 75: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-4.

DD

P-2

24

S

uppl

emen

tal

Pro

gram

s

PRO

GR

AM

TIT

LE

AN

D F

UN

CTI

ON

h) do

RC

A-1

10

A/D

DP

-22

4

INT

ER

FA

CE

(2

24

Sid

e);

Che

cks

the

IOD

C-6

/DE

CV

fo

r se

nse

bit

pat

tern

s an

d bl

ock

data

tran

srer

.

DD

P-2

24

AR

ITH

klE

TIC

FU

NC

TIO

NA

L T

ES

T;

Tes

ts a

ll a

rithm

etic

log

ic.

r-

IVA

R

DIC

P

DS

AT

DS

CP

DS

DP

DS

MD

DS

RM

DS

SS

DS

TA

DS

TO

- KS

C F

OR

M

DD

P-2

24

CE

NT

RA

L P

RO

CE

SS

OR

TE

ST

; V

erifi

es p

rope

r op

erat

ion

of t

he D

DP

-22

4 l

ogic

ele

men

ts

with

em

phas

is o

n th

e in

stru

ctio

n re

pert

oire

.

AU

TH

E

LE

ME

NT

Ah

RE

SP

ON

SIB

L C

ON

TR

AC

TC

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

GD

C-3

1 IB

M

16

-22

6A

15

691

DIG

ITA

L S

WIT

CH

CH

EC

KO

UT;

Tes

ts t

he o

ptio

ns a

nd c

on:ro

ls

of t

he d

igit

al

switc

h.

DD

P-2

24

ME

MO

RY

DIA

GN

OS

TIC

; V

erifi

es t

he o

pera

tion

of a

ll D

DP

-22

4 m

emor

y lo

catio

ns a

nd

diag

nose

s an

y fa

ilure

s en

coun

tere

d.

RE

FR

ES

Y M

EM

OR

Y D

IAG

NO

STI

C;

Per

form

s a

com

plet

e te

st o

f re

fres

h m

emor

ies,

dat

a pa

tche

s,

and

cont

rol

units

, an

d th

en tr

ansf

er o

f da

ta f

rom

ref

resh

mem

orie

s to

con

sole

s.

SE

NS

E S

WIT

CH

TE

ST;

C

ontin

uous

ly c

heck

s th

e st

atus

of

the

DD

P-2

24

sen

se s

witc

hes.

DD

P-2

24

CO

NS

OLE

ALI

GN

ME

NT

TE

ST

; P

rovi

des

cons

ole

di;p

lays

an

d co

ntro

ls t

o ai

d in

alig

ning

an

d tr

oubl

esho

otin

g di

spla

y co

nsol

e eq

uipm

ent.

TY

PE

WR

ITE

R O

UT

PU

T T

ES

T;

Per

form

s pr

edef

ined

test

s on

the

type

writ

er t

o in

sure

it

is o

pera

tiona

l pr

ior

to v

ehic

le t

estin

g.

LA

ST

R

ELE

AS

E

DA

TE

5-1

2-7

2

5-1

1-7

2

9-1

5-6

9

10

-10

-69

2-2

4-7

0

1-1

2-7

0

1-5

- 7

1

7-2

7-7

0

1-5

- 7

1

UN

RE

LE

AS

ED

PR

OC

RA

M

ST

AT

US

. O

R O

PE

h

CH

AN

CE

DO

CU

ME

NT

S

(CP

CR

-PT

R)

Page 76: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-5.

DE

E-6

C/E

S

uppl

emen

tal

D~

agno

stic

Pro

gram

s

I N

AS

A A

UT

H.

EL

EM

EN

T A

ND

IV

AR

R

ES

PO

NS

IBL

E

1 / .oNT.A

cTo.~

P

RO

GR

AM

TIT

LE

AN

D F

UN

CT

ION

I D

D5

li

OH

51

I DD

54

I

GC

C-2

7 f

PH

OT

O-R

EA

DE

R T

ES

T;

Per

form

s a

furi

ct~

o~

~a

l te

st o

r tl

ie X

DS

93

0 p

aper

tap

e re

ader

.

DD

53

GD

C-2

7 T

ELE

TY

PE

TE

ST;

P

erfo

rms

a te

st o

f tti

c X

DS

93

0 te

lety

pe ~

np

c~t

acce

ptat

~ce a

rid ~

ritc

rpol

atio

n, ou

tput

/

I IBM

1 vali

dity

, an

d ou

tput

tim

ing.

GD

C-2

7 IB

M

SY

ST

EM

TE

ST

; P

erfo

rms

a fu

nctio

n te

st o

f cy

cle

fl~

p-f

lop

s, in

terr

upts

, co

mpa

rato

r co

unte

r, cl

ock,

re

mot

e pa

nel

inpu

ts,

Fra

nklin

Prin

ters

, an

d th

e re

niot

e po

wer

~nd

icat

or. (

DD

51

- X

DS

93

0)

(DD

51/D

H51

XD

S 9

30/R

emot

e X

DS

09

2)

GD

C-2

7 IB

M

I DDbO

""yfi27

1 MAGN

ET

IC T

AP

E U

NIT

DIA

GN

OS

TIC

; Is

olat

es t

o P

C ~

rior

l~rl

cs

,?rit

!'or

~~

~c

cl~

ar~

rca

l/e

lcc

trrc

al

cot~

~lio

t~et

its,

I w

ithi

n th

e X

DS

93

0 M

agne

trc

Tape

Cor

itrol

UIII

~, h

~~a!

jriet

IC

Ta

pe U

nit,

or M

agne

tic T

ape

Dec

k.

PA

PZ

R T

AP

E P

UN

CH

TE

ST

; V

erifi

es t

hat

klle

per

forr

nanc

c of

the

XD

S 9

30

put

~ch

is w

ithi

n to

lera

nce,

an

d th

at t

he r

eade

r IS

fu

nctio

ning

pro

perly

.

GD

C-2

7 1

,BM

I

DD

bl/

/ G

DC

-27

HI/

LOW

SP

EE

D D

AT

A L

INK

DIA

GN

OS

TIC

; P

erfo

rtiis

a c

omyl

etc

diag

~io

stic

clie

ch 8

1 tli

e rr

durld

atit,

hi

gh a

nd lo

w s

peed

dat

a lin

k sy

stem

, be

twee

ll th

e R

emot

e P

rogr

artr

n~ab

lc Sca

rlrle

r (X

Dh

-09

2)

rr1

the

Mob

ile L

aunc

her

-r>d

the

DE

E-6

Com

pute

rs (

XD

S-9

30

) in

the

LCC

.

W-B

UF

FE

R L

INE

PR

IN'T

ER

AC

CE

PT

AN

CE

TE

ST

; V

errf

ies

the

f~rr

~ct

ror~

~rl

q

of t

he a

lplla

nutn

er~c

lrne

pr

inte

r,

whe

n co

rlnec

ted

loca

lly t

o tt

ic X

DS

93

0.

TIM

E M

UL

TIP

LE

X I

..~>M

MU

NIC

ATI

ON

CH

AN

NE

L D

IAG

NO

STI

C;

Isol

ates

any

Ita

rdw

arc

failu

re w

itlii

ti

the

XD

S 9

30

Tim

e bl

trlti

plex

Cor

rirrr

unic

atio

r~ C

finr~

riel (T

MC

C) c

ircu

rtry

.

ny i

1 1

\3

KSC F

OR

M 1

6-2

26

1 1

5 6

9)

* Del

eted

Pro

gram

s

Page 77: JOHN F. KENNEDY SPACE CENTER

Tab

le 2

-5.

DE

E-6

C/E

S

uppl

emen

tal

Dia

gnos

tic P

rogr

ams

:Con

tinue

d)

NA

SA

AU

TH

. E

LE

ME

YT

ANI

RE

SP

ON

SIB

LI

CO

NT

RA

CT

OI

GD

C-2

7 IB

M

Db

65

3D

66

/ O

H6

6

GD

C-2

7 IB

M

GD

C-2

7 I B

M

GD

C-2

7 IB

M

GD

C-2

7

IBM

u--

KS

C F

OR

M 1

6-2

16

A (

5 6

9)

I R

EV

.

SC

AN

SY

ST

EM

LO

GIC

DIA

GN

OS

TIC

; Is

olat

es a

ny h

ardw

are

fail~

rre w

ithi

n th

e sc

an s

yste

m l

ogic

ci

rcui

try.

(D

D13

Rem

ote

XD

S 9

30

) (D

D61

i'DH

61

Rem

ote

XD

S 0

96

)

ME

MO

RY

UN

IT D

IAG

NO

STI

C;

Per

form

s a

deta

iled

veri

ficat

iori

of

the

mai

n fra

me

mer

nory

.

C

2 = 2 II

I

CE

NT

RA

L P

RO

CE

SS

OR

UN

IT D

IAG

NO

STI

C;

Per

forr

r~s a

deb

1 led

ver

ific

atio

n of

the

Cen

tral

Pro

cess

or

Uni

t (C

PU

) fo

r a

ll p

rope

r mac

hine

ins

truc

tion

exec

utio

n.

l2 l2

PR

OG

RA

M T

ITL

E A

ND

FU

NC

TIO

N

I

DE

E-6

RE

MO

TE

1/0

CH

AN

NE

L D

IAG

NO

ST

IC;

Per

form

s a

deta

iled

test

of

all

cir

cu~

try ir

i the

DM

C

and

TM

CC

ass

ocia

ted

wit

h th

e X

DS

-09

2 R

emot

e C

ompu

ter

Sys

tem

.

OW

S

b- 5

RE

MO

TE

CE

NT

RA

L P

RO

CE

SS

OR

UN

I T D

IAG

NO

STI

C;

Per

forr

vs a

deb

1 led

ve

r~f ~c

ati

o~

i of

the

cen

tral

pr

oces

sor

unit

of

the

Rem

ote

Pro

gram

mab

le S

cann

er (

XD

S-0

92).

l1 l

1 sc

anne

r m

emor

y.

I R

EM

OT

E M

EM

OR

Y D

IAG

NO

STI

C;

Per

forr

ris a

de

ta~

led

veri

fica

tion

of

the

XD

S-0

92

rem

ote

prog

ram

niab

le

2

XD

S D

IAG

NO

ST

IC C

ON

TR

OLL

ER

; X

DS

men

lory

, ir

~st

ruct

ion,

PA

S t

ests

11lu

s ex

ecut

ive.

lo

lo 2

DE

E-6

SY

ST

EM

TA

PE

ED

ITO

R;

Fun

ctio

ns d

s an

edi

tor

for

the

UD

EX

Sys

terr

t Ta

pe b

y bu

lldin

g th

e D

iagn

ostic

Sys

tem

Tes

t Ta

pe.

I UNREL

EA

IED

PR

OG

RA

M

ST

AT

US

, O

R O

PE

N

RE

LE

*SE

C

HA

NG

E D

OC

UM

EN

TS

(C

PC

R-P

TR

)

DE

E-6

DIA

GN

OS

TIC

SY

ST

EM

EX

EC

UT

IVE

; P

erfo

rms

exec

ut~

ve fu

nct

~o

r~s for

the

diag

nost

ic s

yste

m

prog

ram

s th

at r

esid

e on

the

mai

nten

ance

test

ta

pe

. It

~t~

clu

de

s all a

uton

iatic

pro

gram

seq

uenc

e ca

pabi

lity.

1

A

1A

Page 78: JOHN F. KENNEDY SPACE CENTER

NA

SA

AU

TH

E

LE

ME

NT

AN

R

ES

PO

NS

IBL

CO

NT

RA

CT

0

CA

P-B

CA

P-B

UD

06

UD

07

UD

08

4

CA

P-B

CA

P-B

CA

P-B

UD

09

UD

TR

CA

P-B

CA

P-B

N

I F

F

Tab

le 2

-6.

DE

E-6

C/E

S

uppl

emen

tal

Uti

lity

and

Pos

tpro

cess

ing

Pro

gral

lrs

SY

MB

OLI

C T

AP

E E

DIT

OR

; E

dlts

DE

E-6

syr

rrbo

lic t

apes

/ 2

1 2 ( 6

-30

-71

/ T

AP

E D

UP

LIC

AT

OR

; C

opie

s B

CD

or

I111

1ary

tape

to

pape

r ta

pe;

dupl

icat

es p

aper

tap

e.

UP

23

UP

24

DE

BU

G A

ID;

Pro

vide

s su

ch d

ebug

y~ny

fur~

ct~

o~

is

as -

add

ress

~i~

od

ific

at~

o~

i,

core

dun

rps

- ins

truc

tion

trac

es -

loop

con

trol

s et

c.,

for

nlai

~ite

riarr

ce a~

id dc

velo

prrr

er~t

of D

EE

-6 )

~ro

yra

~~

is.

UN

RE

LE

AS

ED

PR

OG

RA

M

LA

ST

/ ST

AT

US

, O

R O

PE

N

RE

LE

AS

E

CH

AN

GE

DO

CU

ME

NT

S

DA

TE

I

(CP

CR

-PT

R)

PR

OG

RA

M T

ITLE

AN

D FUNCTION

CA

P-B

CA

P-8

FO

RT

RA

N D

UM

P P

RO

GR

AM

; U

sed

to d

u111

l) all

FO

RT

RA

N p

roqr

atl,s

to p

aper

td1)

c or

rr:a

yrre

t~c t

ape

rn

SY

MB

OL

or M

ET

A-S

YM

BO

L fo

rmat

. lA I

A I 12-

3-71i

-

-1

2

'cS

C F

OR

M 1

6-22

6).

15 6

91

RT

FO

RT

RA

N ll

MO

NA

RC

H T

AP

E E

DIT

OR

PR

OG

RA

M;

Bui

lc!s

all[

! LI

ON

AR

CH

tape

s fo

r th

e 3

/ 3 1 3-1

8-7

1

1 D

EE

-6 s

yste

rn b

, ad

dlriy

rec

ords

fro

rx ~

~ia

qrre

tlc or p

aper

tap

e or

or

1ttl1

1(1 tc

cord

s fro

91' r:

~ayr

retlc

taoe

. I I

RE

V.

DE

E-6

TA

PE

LIS

T P

RO

GR

AM

; L

ists

SY

MB

OL

arld

ME

TA-S

YP

AB

OL

I~s

t tape

s 011 th

e 1

60

colu

cnn

linep

rint

er.

10 I o

I 11-6-7

0~

g z -

P 2

DE

E-6

P

AP

ER

TA

PE

GE

NE

RA

TOR

; G

er~

c~

~tc

pa

per

tape

o~

ll;)u

t 011

the

DE

E-6

BD

S 9

30

. 11

1 1

/ 5-2

1-7

1

(

X

11

-5-6

9

TA

PE

LIS

T D

UM

P;

Dum

ps D

EE

-6 s

y~nb

ol an

d fo

rmat

ted

sym

bol

list

bp

es

and

alp

hanu

nler

ic t

apes

. 1 4

1 4 11 1

-18

-69

1

SC

63

OP

ER

AT

ION

AL

SC

AN

PR

OG

RA

hl S

IMU

LAT

OR

; L

ists

sto

red

d~

scre

te ev

e~rt

s from

a s

irnul

atio

n te

st p

rofi

le r

elat

ive

to c

lock

par

arrle

tcrs

to

sl~

~l~

rla

te

vehl

cle

r~ia

lfur

icti

o~is

an

d oc

curr

ence

s fo

r la

unch

cre

w

trai

ning

.

1

TA

PE

ED

ITO

R;

Pro

vide

s a

mea

ns o

f ed

itiny

DE

E-6

sys

tem

tap

es,

and

coin

parir

ig a

nd q

e~ie

rat~

riy DE

E-6

ID

ta!)l

es f

rorr

i tlie

G.E

. IC

D ta

pe v

ia A

TO

M 0

11 tl

ie R

CA

-1lO

A

com

pute

r.

0

41

( 9

5-7

-71

6-3

0-7

2

Sub

rout

ines

UV

SS

Page 79: JOHN F. KENNEDY SPACE CENTER

Ta

ble

2-6

. D

EE

-6 C

/E S

uppl

emen

tal

Uti

lity

Pos

tpro

cess

ing

Pro

gram

s (C

ontin

ued)

NA

SA

AU

TH

. 1

EL

EM

EN

T A

N0

R

ES

PO

WS

IBL

E

CO

NT

RA

CT

OR

P

RO

GR

AM

TIT

LE

AN

D F

UN

CT

ION

UP

26

Z D

il D

ZD

lT

ZD

TM

ZD

SC

CA

P-B

GD

C-2

7 C

AP

-8

GD

C-2

7 C

CS

D

GD

C-2

7 C

AP

-B

CA

P-B

RC

A-1

1O

/DE

E-6

S

EQ

UE

NC

E T

AB

LE

GE

NE

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