nasa · 2015. 3. 9. · msc internal note no. 69-fm-137 project apollo apollo mission f...

., --..

MSC INTERNAL NOTE NO. 69.FM.137

.:'

00/99Unclas16270

MSC INTERNAL NOTE NO. 69-FM-137

PROJECT APOLLO

APOLLO MISSION F (AS-505jCSM-I06jLM-4)SPACEC RAFT OPERATIONAL TRAJECTORY, REVI SION 1

VOLUME II - TRAJECTORY DATAPART 3 - FLIGHT CREW SIMULATOR DATA

By Ron D. Davis and Larry D. DavisFlight Analysis Branch

May 12,1969

MISSION PLANNING AND ANALYSIS DIVISION

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

MANNED SPACECRAFT CENTER

HOUSTON, TEXAS

Approved:~~. (l~_Charlie C. Allen,hiefFlight Analysis Branch

Approved:~~j.J~~~~~-¥:'=~ __JohnMiss

TABLES

Table Page

-I MISSION-DEPENDENT CONSTANTS

computed from weight

(a)(b)(c)(d)(e)

Launch data .Thruster data . .Center of gravityAerodynamicsCross-section area . ... .. ..

557

1011

II CSM RESET VECTORS

(a) Evasive maneuver(b) MCC-l maneuver(c) LOI-l maneuver(d) LOI-2 maneuver(e) Separation maneuver(f) DOl maneuver(g) Phasing maneuver(h) Insertion maneuver(i) CSI maneuver(j) CDH maneuver(k) TPI maneuver(1) TEl maneuver(m) Entry. • . .

III 1M RESET VECTORS

(a) DOl maneuver(b) Phasing maneuver(c) Insertion maneuver(d) CSI maneuver(e) CDH maneuver(f) TPI maneuver

IV CSM .REFSMMAT

. .

12131415161718192021222324

252627282930

(a) Launch through MCC-3maneuver. . .(b) Mcc-4. maneuver .through Mcc-6 maneuver(c) MCC-7 maneuver through entry .

V CSM NAVIGATION UPDATES

(a) Evasive maneuver(b) MCC-l maneuver

iii

313233

3435

Table Page

(c) LOI-l maneuver · . 36(d) LOI-2 maneuver 37(e) Separation from 1M 38( f) TEl maneuver . 39

VI LM NAVIGATION UPDATES

(a) DOl maneuver 40(b) Phasing 41(c ) Insertion 42(d) CSI maneuver 43(e) CDH maneuver 44(f) TPI maneuver 45

VII DETAILED MANEUVER TABLES

(a) Evasive maneuver 46(b) MCC-l maneuver 47(c) LOI-l maneuver · 48(d) LOI-2 maneuver · 49(e) Separation from 1M 50(f) DOl maneuver . 51(g) Phasing . 52(h) Insertion maneuver 53(i) CSI maneuver 54(j ) CDH maneuver 55(k) TPI maneuver 56(1) TEl maneuver 57

VIII FDAI ANGLES FOR 1M MANEUVERS 58

IX CSM EXTERNAL ~V UPDATES

(a) Evasive maneuver 59(b) MCC-l maneuver 60( c ) LOI-l maneuver · 61(d) LOI-2 maneuver 62(e) Separation from 1M 63(r) TEl maneuver · 64 ..,

X 1M EXTERNAL ~V UPDATES

(a) DOl maneuver · 65(b) Phasing maneuver 66

iv

Table Page

(c) Insertion maneuver 67(d) CSI maneuver 68(e) CDR maneuver 69(f) TPI maneuver 70

XI MANEUVER PADS

,.. (a) Evasive maneuver 71(b) MCC-l 72(c) LOI-l 73(d) LOI-2 . . . 74(e) Separation from 1M 75(f) DOl 76(g) Phasing TT(h) Insertion 78(i) CSI 79(j) CDR 80(k) TPI 81(1) TEl 82(m) Lunar entry 83

v

.....

"

'w

APOLLO MISSION F (AS-505/CSM-106/LM-4)

SPACECRAFT OPERATIONAL TRAJECTORY, REVSION 1

VOLUME II - TRAJECTORY DATA

PART 3 - FLIGHT CREW SIMULATOR DATA

By Ron D. Davis and Larry D. Davis

SUMMARY

The data in this document are compiled to satisfy flight crew andflight controller training and simulation requirements for the F mission.This data pack is based on a F mission operational trajectory, revision 1(ref. 1). This document contains reset vectors, REFSMMAT updates,navigation updates, navigation checks, detailed maneuver tables,entry data, and associated flight crew data.

INTRODUCTION

The nominal Mission F plan involves the following mission phases

1. Launch, which ends with insertion into earth parking orbit.

2. Earth orbit coast, which ends with TLI.

3. Translunar coast, which ends with LOI.

4. Lunar orbit operations, which ends with TEl.

The prime objective of this phase will be to demonstrate allphases of Mission G except those which directly involve LM powered descentand powered ascent. These operations will include a LM-active rendezvous.

5. Transearth coast, which ends with entry into the mid-Pacificrecovery area.

The total mission duration will be approximately 8 days. Thedata presented in this document were computed by the use of the RTACFprocessors.

AGS

ALPHA

APS

CD

CDH

CL

CM

CSI

CSM

cg

DOl

DPS

DSKY

EECOM

EL

EOI

ER

FDAI

GET GEN

g.e.t.

G.m.t.

GMT ID

I sp

2

ABBREVIATIONS

abort guidance system

angle of attack

ascent propulsion system

coefficient of drag

constant differential height

coefficient of lift

command module

coelliptic sequence initiation

command and service modules

center of gravity

descent orbit insertion

descent propulsion system

display keyboard

electrical, environmental, and communications

earth launch

earth orbital insertion

earth radii

flight director attitude indicator

time of data generation

ground elapsed time

Greenwich mean time

identification of time

specific impulse

"

LES

LGC

LM

LOl-l

LOI-2

PAD

RCS

REF

REFSMMAT

RTACF

8 and S

8LA

8M

8PS

STA lD

t

TEl

TEC

TlGN

TLC

TLl

TPF

TPl

WT

w

3

launch escape system

lunar module guidance computer

lunar module

lunar orbit insertion

circularization maneuver after LOl-l

pre-advisory data

reaction control system

reference body

reference to stable member matrix

Real-Time Auxiliary Computing Facility

start and stop

spacecraft/LM adapter

service module

service propulsion system

station identification

time

transearth injection

transearth coast

time of main engine ignition

trans lunar coast

translunar injection

terminal phase finalization

terminal phase initiation

weight

flow rate

4

RESULTS

A set of data that consists of the following is provided foreach of the Mission F maneuvers (or entry); reset vectors, REFSMMATupdates, navigation updates, navigation checks, detailed maneuvertables, and other required flight crew data. This data pack supersedesall earlier F mission data packs.

A brief summary of mission-dependent constants used in thegeneration of this document are presented in table I. A more detajledtabulation of mass properties data can be found in references 2 and 3.

The CSM and LM reset vectors for each maneuver and entry are containedin tables II and III. These vectors are in the mean Besselian coordinatesystem. This system can be defined as follows: an inertial Cartesiansystem with origin at the center of the reference body (earth or moon)with the X- and Y-axes in the mean equatorial plane and the Z-axiscoincident with the mean polar axis (positive to the north). TheX-axis is alined at the intersection of the earth's equatorial planewith the ecliptic at the nearest beginning of a Besselian year.

The CSM and LM REFSMMAT update quantities for the various phasesof the F mission are contained in table IV. The required navigationupdates for the various maneuver sequences are presented in tables Vand VI.

The "detailed maneuver table" quantities for each of the plannedmaneuvers are presented in table VII. A tabulation of LM gimbal anglesconverted to LM FDAI angles is given in table VIII. The external ~Vupdates for each of the maneuvers are presented in tables IX and X.Additional information in the form of pre-advisory data (PAD) isprovided in table XI.

ff

I

5

TABLE 1.- MISSION-DEPENDENT CONSTANTS

(a) Launch data

Date of launch. May 18, 19h9

G.m.t. of launch 16:49:00

(b) Thruster data

SPS steady state

..

Thrust, IbW, Ib/secI ,sec.sp

SPS tailoff ~

Burn time, sec .Thrust, Ib~, Ib/secI ,sec.sp

SM RCS (per quad)


CM RCS (per quad)


1M RCS (per quad)


APS steady-state

Thrust, IbW, Ib/secI ,sec.

sp

20 50065.162314.60

0.5920 847.5

66.590313.07

102.80.371

277.09

96.00.353

271.95

100.00.367

272.48

3 500.011.427306.29

APS tailoff

Burn time, secThrust, lbW, lb/secI , sec .sp

DPS onboard (92.5%)

Thrust, lbW, lb/secI , sec .sp

DPS (40% level)

Thrust, lbW, lb/secI , sec .

sp

DPS (10% level)

Thrust, lbW, lb/secI , sec .

sp

DPS tailoff

Burn time, secThrust, lbW, lb/secI , sec .

sp

6

0.12990.0

9.65309.84

9712.532.270300.98

4200.013.952301.03

1050.03.488

301.03

0.386503.020.080301. 44

7

TABLE I.- MISSION-DEPENDENT CONSTANTS - Continued

(c) Center of gravity computed from weighta

[CSM propellant on bottom of tanks]

WEIGHT X Y Z PITCH TRIM b YAW TRI MbLB INCHES I NCHE S I NCHE S DEG DEG

23200.00 983.59 -2.82 8. ('1 -3.05 -1.0125400.00 9"71 .9R -1.61 1.45 -3.01 -0.6621600.00 962.~17 -C.59 6.98 -3.08 -0.2629800.00 956.14 0.28 6.58 -3.06 0.1332000.00 951.;>7 1.02 6.23 -3.02 0.5034200.00

8

TABLE 1.- MISSION-DEPENDENT CONSTANTS - Continued

(c) Center of gravity computed from weighta

- Continued

[1M with APS and DPS propellant on bottom of tanks]

WEIGHTLA

1400,1. or145('n.n('\1500J."0155GG.rn16()(,C.00165C'D.rn17(':O".no115~O. 00180)"'."1'1 fl 5')1:. rr19000. (.10IG50U.C"21'!)'ln. 'r20 '51)0. '10210 n ').,,071 5n". "0?200 ').nn2251),~.~C

2~C)('.('O

2'3511. rn241'1'):'.002450(1. ''''7

TABLE I.- MISSION-DEPENDENT CONSTANTS - Continued

(c) Center of gravity computed from weighta - Concluded

[1M with APS and DPS propellant on top of tanks]

WEIGHT X Y Z PITCH TRIM b YAW TRIM bL8 INCHES INCHE S INCHES DEG DEG

19500.00 202.53 -0.46 -0.64 0.76 -0.5420000.00 201.63 -0.45 -0.63 0.75 -0.5420500.00 200.73 -0.44 -0.61 0.75 -0.5421000.00 199.84 -0.43 -0.60 0.75 -0.5321500.00 1'18.99 -0.42 -0.58 0.74 -0.5322000.00 198.12 -0.41 -0.57 0.74 -0.5322500.00 1 'H. 25 -0.40 -0.56 0.74 -0.5323000.00 196.38 -0.39 -0.55 0.74 -0.5323500.00 195.56 -0.38 -0.53 0.74 -0.5324000.00 194.69 -0.37 -0.52 0.74 -0.5324500.00 193.85 -0.37 -0.51 0.74 -0.5325000.00 193.02 -0.36 -0.50 0.74 -0.5325500.00 192.20 -0.35 -0.49 0.74 -0.5326000.00 191.37 -0.35 -0.48 0.74 -0.5)26500.CO 190.53 -0.34 -0.41 0.74 -0.5321000.00 189.72 -0.33 -0.46 0.75 -0.5321500.00 1e8."91 -C.33 -0.46 0.75 -0.5428000.00 188.09 -0.32 -0.45 0.15 -0.5428500.00 181.26 -0.32 -0.44 0.76 -0.5429000.00 186.41 -C.31 -0.43 0.76 -0.5529500.00 185.64 -0.30 -0.43 0.77 -0.5530000.00 184.81 -0.30 -0.42 0.78 -0.5630500.00 183.99 -0.29 -0.41 0.79 -0.5631000.00 183.58 -0.29 -0.40 0.18 -0.5631500.00 183.23 -0.29 -0.40 0.78 -0.5632000.00 182.88 -0.28 -0.39 0.78 -0.5632500.00 182.55 -0.28 -0.39 0.77 -0.55

[Ascent stage with propellant on bottom of tanks]

5001."0 267. 62 '),13 5.94 "~ c.55("0."(\ 262.72 ".11 5.4r r.60"()."C' 25'l.15 j. U: 4.95 ". r.65('0.0r 254.53 1.0 0 4.57

~ c.7"N).Cr, 251.79 ).e8 4.24 I" c.750".,,( 249.65 0.07 3.q~ J. 0.8000.0C 247.99 ').07 3.71 !") O.8500.0C 246.71 ).06 3.49 ", C.901'0.CO 245.74 ) • :: 5 3.3C ,; c.95C".00 245.04 ;.05 3.13 " C.10n OO.Cr 244.57 ').°5 2.97 ". r.

[Ascent stage with propellant on top of tanks]

5"" 1;. er 26" • 51 0.20 1.'12 r.5

10

TABLE 1.- MISSION-DEPENDENT CONSTANTS - Continued

( ) d. ad Aero ynarnlcs

= 1040.90; Ycg = -0.20; Z = 5.80; Weight = 12 121.50 Ib;cg

~x = -100.35 inches; Bank angle bias = -1.97°]

.,14 r H ~.' 4l t) '--l,\ L C) CLIC )I, • \. .

",,), ..., 1 '7" ':45 ? ~ 1F' ) .R.? ':JP' J. 2 R )57• • ~ ·~ .-t" I, ," 1 t, 7 (, ~ ; l 41

., ,..,;\':) .',. 7 3 ') 2 73 )'"• , · " • ,~ t. • I •

7"', 1 t, .:, .- 1, ) c;

~ 1 '=I " 9 'l '")1 2 :I 2 "i '1 n• ·, · ·........ t"'\ 1-, " '~ 1 " 3 , 1 p.-; , ,; 7 ,

11

TABLE 1.- MISSION-DEPENDENT CONSTANTS - Concluded

(e) Cross-section area

CSM, ft 2 129.4

CM, ft2 129.4

LM, ft 2 200.6

APS, ft 2 200.6

(f) Mass properties, spacecraft weight - See reference 3

12

TABLE 11.- CSM RESET VECTORS

(a) Evasive maneuver

(~EAN 6_;S_§J LI AN)EARTH REFERF-NCED

GET ;;

13

TABLE 11.- CSM RESET VECTORS - Continued

(b) MCC-1 maneuver

t·l"tf AN.S.E5.S.1I.-1ANJEARTH REFERENeEn

GET = 9 HR ~6 MIN 46,38 SEC

-- x. -A._--._._.l'I.,.4~l5-tJ1O .. ET-Y z 2~~S8~'2e,OO FT

Z z 14 9940 9 78,00 FT

XoQT·.!- .~ 4~3A.t 7.5. Frl SEc

Yoor = 67~~.25 FT/SECZOOT = J680.61 FT/SEC

.. _. X. -..-. i.. e .3..t12481625.4 8 f R

Y = ~2.261'665197 ER

l ; 7.~65J854647 ER

.......... ~pOl. =. .. ...?4~~.~-'-::57'3ER/HR

YOOT = 1.1'J~1.866.~4 ER/HR

~OOT =. ~J~,Q05560 ERI HR---. ----. WT .-. ~-- ... - .. ----~U.2! , 6O. I..-B .-

14


(c) LOI-1 maneuver

(~~AN 6E.S~lLIA.N)

L,UN'R REFERtNeED ,

GET = 14 HR 4~ MIN ,00 SEC

X ;: .. 15309~7'-.12 f'T

Y : "'1 369 4786,15 FTZ I: p. 8 513J;56,87 FT

XcOT :I 1~7'JA~ FT/SEC

YeOl I: 44 39,36 FrlSEC

ZeOT I: 2379,54 FT/SEC

X I: ·,7)16096649 E~

Y l: "'t6544~70191 ERZ ;: .,4068356864 ER

XCOT I: 12~6~'t~6~.6 ER/HR

Year I: ,7637346163 ER/HRZOOT I: ,409J660419 ER/HR

WT II 9Z~2A,no l..s

15


(d) 101-2 maneuver

(~EAN BESSILIAN)l.lJNAR REFERENCED

''-

GE: T :: 79 HR 11 ~1 I " ,00 St:C

X :: 1122'74.~6 FT

Y .. ,,6121 706,00 Flf..Z :: ..2526~69.66 FT

XOOT :: -~884.16 FT/SEC

Vo°'T :: "683,48 FrlSEC

ZOOT .. -J73,33 FrlsEC..X :: ,053b456527 ER

V :: -,292~~4:5J14 ER

Z :: -,1207206966 ER

XoOT :: -,8402~62216 ER/HR

"'OOT :: -,11 7SH424 7 1 ER/HR

ZOOT :: -,06 4 2265659 ER/HR

WT :: 68"67.15 l.a

16


(e) Separation maneuver

(~t;A.N BE~ lLlAN)~UNAR REFERENCED

GET • 97 HR 3' Mr t\! .00 SECX = ..~_O 5~ ~ 71 •62 FTV • 109~6'.14 FTZ = .6403'.54 FT

XOOT = 66. 93 FTlsECVeOT =: 4~37,:?3 FT/SEC

ZOOT • 2056,68 FT/SECX = "',28 92214209 ERV • ,00 52)12201 ERZ c "',00 3 0602286 ER

XeO T • ,°t1~_~ ~'7~_? ER/HRVeOT ;: .84 9JtSS6415 ER/HR

ZeOT • ,3538256884 ER/HRWT = 6I~8'5,Q6 LoS

17


(f) DOl maneuver

O~E4N BE6S1Lt AN)~UNAR REFEREN~ED

'Ii

GET : 99 HR 14 MIN .00 SEC

X = .'160406,16 FT

V : .,47'12651,00 FT

Z = .2031801,4' FT

XoOT = "'4'62,92 FT/SEC

VOOT = 2609,11 FT/SEC

ZOOT = 100:5,69 FT/SEC

X = "',151C~96166 ERV = "',22664 19958 ER

'l II -.0970 9 60967 ER

XDOT = ·,784991:5910 ER/HR

YOOT = .44e8 640055 ER/HR

ZDOj = .1726 716720 ER/HR

VlT = 36414,12 LB

18


(g) Phasing maneuver

(~EAN BESSILIAN)L.l.. NAR REFERENr.ED

GE:.T = 100 HR 26 Mhl ,00 nEe)( = 569266~,C;O F'f'

V = 1866233,95 F"T

Z = 880054,66 FT

XeOT = 161',43 FT/SEC

YeOT = "'4654,1J4 FT/SEC

ZeOT = -1904,93 FT/SEC

X = ,2720'013836 ERY = ,0891 8 36630 ER

Z = ,0420'60814 ER

XCOT = ,31266S63 R7 ER/HR

YeOT = ",6006676137 ER/H~

ZDOT = .. ,32 77175674 ER/HR

WT = 36 4 74.12 LB

19


(h) Insertion maneuver

(MEAN BESSiLIAN)~~NAR REFERENeED

",.

GET : 10~ HR a3 MI~, .00 SECX II 55°8380.)7 FT

y ;I 226'2.13.134 FT

Z = 1051145.53 FT

XoOT II 2216.93 FT/SEC

, YOOl ;; -4'05.88 FT/SEC

ZeOT ;I ·~~36.19 FT/SEC

X II .263Z347010 ER

Y II ,lQ9Z011128 ER

Z II ,0502321846 ER

XOOT ;II ,381'9385:56 ER/HR

YOOT • ",17'178'548 ER/HRZOOT • -,'1"9.2e268 ERIHR

WT ;I 36474,12 ~B

20


(i) CSI maneuver

(ME.AN BESSILUN)I..UNAR REFEReNcED

GET II 100l HR 1~ MIN .00 siC

X • -,926831 ,00 FTV II .. 4224122 69 FT-- .z ;: .. 183D011.25 FT

)(OOT II .. 4e11.13 ,"'SECVCOT II J231.20 ","SIC

ZOOT II 1211.93 FT/SiC

X • -,181"55569 ERV • "',2011625451 ERZ II -,0814'26510 ER

XOOT a ~,100;JaJ9681 E~'Io4R

VOOT II ,'5"152'117 ER/HR

ZoOT ;; ,a18819'612 ER/Io4R

WT • J.~14.12 loB

..

21


(j) CDR maneuver

(MEAN 8E&SJ~IAN)~UNAR REFERENeEO

GET • S.04 HR 12 MhJ .00 SECX • 3601290.09 FifV • 4467148.94 F'Z • 192"2. •• 1' ,IfXOOT I: 4291,1. ~T/SEC

VOOT • "2~69.01 ~'/5EC

ZOOT ill -1158.86 F1'/SEC)( • ,2.124331118 IERV • ,Z134162928 ERZ • ,0920S,6!U19 ER)(OOT • ,138;)38 •• 81 ER/IoIR

VeOT I: -.'101fJ992'. ER/HR

ZOOT I: -,199J67!288 ER/HR .

WT • 364'4.12 Le

22


(k) TP1 maneuver

(MEAN BESSILIAN)~U~AR REFERENCED

GET = 104 HR 49 '1 I N 36.00 SEC

X = 2954:51 8 '16 F'T'

Y = ... 489;5702 44 FT•Z = "1964 615.17 FT

XOOT = "'4670.21 FT/SEC

YeOT = -2'80.14 Fi/SeC

ZeOT = "1075.~8 FT/Sec

X = ,14111:110141 ER

Y = -.2;5386044RQ ER

Z : -,09 4 8408972 ER

XOOT = .. ,80344922~4 ER/HR

Yt;OT = -.40 95758647 E~/HR

ZeOT ;: -,3.85091~8CJO ER/HR

WT = 36 4 74.12 Los

23


(1) TEl maneuver

ib'.f.AN-aES.5 ~- tAN,) --._-~UNAR REFeRENeED

GET II 136 HR 2D MI~ .00 SEC

)(-- ...L ··----~... ii96_:!_t -'-5''£.T

Y c e3807~8~.09 FT .

Z = -150V2S1,'O FTX-S0T ~... - -- _- ~J_~U.79 ~!ISiC

YeOT • -Jtl1.56 FT/SEC

ZoOT • -1"1,00 FT/SEC

X II _.__ - ....~VQ!;,'tJ92 ER

Y II

z •. XCQT.II

veQT •

ZOOT •

- --'---_. WT-- =

·.1819~259?O ER

~.07207.66699 ER

.~ ...~Z2~~2..54'1 ERlHR

·,~21J2243A1 ER/HR

• ...270,70.3401 ER/HR

.____._J.O 6 63.. Z9-LB- ..

24

TABLE 11.- CSM RESET VECTORS - Concluded

(m) Entry

( f' EAN 8ESSI LIt:.. N )EARTH REFERFNCED

H:T = 191 HR 31 '1 I 'I '00 SEC

X : -223~1t19S.75 FT

y ;: -2 7 107 131).'5 FT

l. : -1399917'i.P.7 FT

>- COl : cl1J~.43 FT/SEC

YL,;CT : "36"),07 FT/SEC

ZCOT : 1U74.46 FT/SEC

X : -1. i)6 9 :.,tl69:S27 ER

y : -1,2953 9 062 6 0 CoR

! : -,66 891J 2(n66 EP

Xl;OT : 4.6b2J917l:i~b ~R/HR

YCCn : .4J6C19Ci2 n O ER/HR

ZeOT : .184b 4 75356 ~R/HR

WT : 24581.0 L.R

25

TABLE 111.- LM RESET VECTORS

(a) DOl maneuver

(MEAN SEI'ILIAN)~UNAR RE'IRENeED

GET • 99 HR ~_ MIN ,00 SEe

)( III

Y ;;

z •)(OOT I

YOOT-

lOOT •)( .Y II

z •XOOT 11

YeOT I:

ZOOT II

WT •

.31"65,,61 .T••7.8~5',12

".aO:)4202,'7"·.'64,25 '1151t:

a~0,.20 'Tille2,001.20 FT/SIC

-,1'0".'144 E-",a26'a88264 ER

"'.0912tO!442 ER

'"'.7152"883'9 iR/""R

, 441'4'61666 ER/IolR

It12~~4021" ER/""R

36484,00 loB

26

TABLE 111.- 1M RESET VECTORS - Continued

(b) Phasing maneuver

(MiAN BESSILI'N)~UNAA RE'ERENeEO

GET , 100 \l4R a6 MIN ,DO ~EeX • ~164995.a7 ,,.V ;; 'Z94554,19 ,,.Z , 6J9~28.96 ,tXPOT : 1350.'7 'T/SEC

VcOT • ....984.~1 'T/S£CZeOT -= -2051.16 ,,./8£C

)( :; ,2659'0241J2 E~

V I; ,061'6420'10 E~

Z 11 .030l57'1,932 ER

XOOT • .2l2J'2d9!6 ER/IolRVcOT • ·,8~1'88805l ER/~-ZeOT • ·."28148788 (R/MR\tiT :; )1069,90 LB

27

TABLE 111.- LM RESET VECTORS - Continued

(c) Insertion maneuver

(MEAN BISSILIAN)~UNAR RE'IRENeEO

G~T • 1o~ HR 23 MIN ,DO SEe)( • -'ZI12i. ~H "v • 3940"1.06· ,'"Z • 111"06,14 FT)(eOT • J~8',22 F'r/IICveo' • ·~~48.'9 'T/SECZOOT , -l'J9,'2 ,t/SEC)( • ,206'1"426 E~y I ,188J112118 (fit

Z ;; ,082i5211'1 iR

)(eOT • .'99"12997 ER/\oI~VDOT • ... 6620~6D424 ER/\oIRZOOT • ·.2641:S6!U60 ER/\oIRWT • 30618.'0 LB

28

TABLE 111.- LM RESET VECTORS - Continued

(d) CS1 maneuver

GET • 10~ ~R 2,' MiN ,00 SEex • ·'Oz,~o•• e1 ItTy • .4660~'S.9, FTZ • -199"69.!2 FT)(DOT II .'67ZaS.D "/SEC

YeOT I 2'11. " "/IIC

ZeOT :I 9. ,. ""/SEC. 1.X II ·,1'477'1'" E~

'1 II "12221a'!l100 IR

Z • .. ,O'5~'956t9 ER)(eOT II -I eO:H 144686; ER/HR

YOOT " 1',ZQe6!2" E~/~PtZeOT ;: .16'J9 14154 illt/~_

WT • 82'2. 80 L.B

29

TABLE 111.- 1M RESET VECTORS - Continued

(e ) CDR maneuver

(MIAN BE&'ILIAN)~UN'~ RE'IRENCID

GET " ~O. ~R 12 MIN ,DO sre)( It '0'7671.19 "Y It 410'019.00 FTZ ;: 201'!:H .12 'TXCQ' " .626.05 'T/81eYCOT iii "'2'82.'1 FT/SEC

200T • .991.81 FT/SEC)( II ,146~20i6n8 E~

y I .ia4,.).,62 liltz !II ,Q962704942 ER)(OOT • •"'1'12'06 IR/~'"YoOT • "',444a011070 ER/~RZOOT • ,,,,,, 10••'iI16 e:llt/~.WT • "9,.90 L.B

30

TABLE 111.- LM RESET VECTORS - Concluded

(r) TP1 maneuver

(MEAN 8ES5ILI4N)L.UNAR Re'ERENCED

GET • ~O4 IoIR 49 MiN ".00 SEe)( • )1820'.,47 ,,.Y = ~4671600t~O FTZ , -1887 936,"J ,,.XOOT I "4'~9 •• 9 '''/I,C

YOOT • -262'. !U "/SIC

ZeOT :; ·"~".~8 FT/SEC

)( .. .2.~206J66'8 ERY • -.2232 11 '6321 ERZ ;: -,O90220~OO6 EFt

)(COT III -.'84.002168 ER/IoIIlt

VpOT II: -,4520a96119 ER/~~

ZpOT • -.Z024".'492 ER/~~

WT • '"9~,10 L.B

31

TABLE IV.- CSM REFSMMAT

(a) Launch through MCC-3 maneuver

[Earth orbit insertion]

Fe T OSKV DECIMAL.

XIX~ 6:3113 ",80333900XIXE 41400

XIVE 10J66 ,5301 3910XJVE J4142

XI~E 04256 ,2 712 899 0XJZE 15012

VIXE 011 7:5 ,07758620'fIXE 22604

VIV~ 1Q!)5? ,544837 60VJVE 11721

YIZE 62'10 .. ,A3494450VIZE .42:55

ZlXE ~!> 43~ .. ,5 9044620ZIXE 42044

ZIVE 65465 ",,6496 9520ZIVE 662J~

ZIZE 70255 .. ,4788 2 090ZIZE 57'61

32

TABLE IV.- CSM REFSMMAT - Continued

(b) Mcc-4 maneuver through Mcc-6 maneuver

[Lunar landing site]

FeT DsKV DFCtMAL

XPE 17152 ,9505 474 0XIX!: :54231

XIVE 73244 .. ,2924 6010XlvE 45255

XIZE 76247 ... 10 45'0 90XIZE 6566:5

VIXE 77566 ""n1675490YIXE 67632

VIVE 7166:3 .. ,:584:5 648 0YIVE 51045

YIlE 16011 .92302920'''I ZE 16442

ZIXt. '13023 -,3101 2720llXE 56007

ZIYE 61 77 2 .. ,8756 3160ZP'E 72333

ZIlE 720 4 6 ",,37025720lIlE 73221

33

TABLE IV.- CSM REFSMMAT - Concluded

(c) MCC-7 maneuver through entry

FCT D5KY DECIMAL

XIXE 15153 .825:>9312XIXE 10221

XIYE 10021 .5U2085~.3XIYE 02553

XIZE 04075 .2574997SXIZE 16010

YIXE 77733 -.OU4S019~YIXE 43662

YIYE 07312 .4021912L1YIYE 10516

YIZE 61637 -.8t)b-'688dYIZE 62667

ZIXE 66701 -.5042~79'tZIXE 65622

ZIYE 135~.3 .7.3095103ZIYE 36333

ZIZE 06110 .3d3d422~ZIZE 157~0

34

TABLE V.- CSM NAVIGATION UPDATES


)( OO,~, 1.8403574.0'X 05741

V 01'5, 9,3?666tC·07V 0163t

Z 0104:! 5.8ro11~6"'07Z 2625~

X"'~CT 7442~ p.4,537R463+03X"'r'lC T 6261C

V"OCT 11:>4C 1.2113619·04V"'f)C'T 0762~

Z-nc T 0544' 7,320021 4*0 3Z"DCT 3346~

,.00136 A 16 47,56

T 0122~

35

TABLE V.- CSM NAVIGATION UPDATES - Continued

(b) MCC-l maneuver

36

TAB1E V.- CSM NAVIGATION UPDATES - Continued

(c) 101-1 maneuver

)( 77J1C ~8,31141035"O~X 71;'71

V 00007 2,0 739391"'0 5V 2673:!

Z 777JJ? "8,65 92552"'0 5Z 7100~

X-DCT 14:30~ 4,0638651·03X--reT 37034

v.. rCT 2~~S4 5,2 17646 9+03V-reT o 22

Z-DCT 112614 3.06838n2·0JZ... neT 16061

T OJi 74 7S :n 43'1 7T 11 1~

37


(d) LOI-2 maneuver

X 7747~ "5.1 9 56790+06X 6551?

" 0016( 3.0127.22"0 6" O:3G:3r.Z OCU5~ 1.1586&10"'06'l. 0;344('

X-De T . 11121 3,0')52858"'03X-DCT ,nO!

""'DCT 14533 4 .159~H26.03Y-DCT 12 421

Z-D'CT 05341 1.7 A51 8t42+03Z-nCT 35232

T 0333~ 79 '38 45.52i lJ~5C

38


(e) Separation from LM

)( 0027~ 5,OQ3 4 732*06)( 20J2~

y 00151 2.9 A74014"'06If 0410 4

Z 000 61 1.33598 19.0 6Z 2651'

X-nCT 10 634 2.8092:591'*03X"DeT 34044

y-DCT 6~~1? t"4.1'30C 77 +0)Y-OCT 6642~

Z"DCT 7267';. "'1.6 R50430"'03Z-nCT 5345.,

T 042. 61 98 ?-3 15 ,62T 32652

39

TABLE v. -' CSM NAVIGATION UPDATES - Concluded

( f) TEl maneuver

x_ 71H:.Z- -5 .. 9666077·06X 4000~

Y 00044 9.6'63251·05Y 00055

Z- 0001~ . 2.2100952+0 5Z 01501

XO!'DCT 02552 8.8~54185·02X~bC'T ~4'Ot

- y"DCT __ 1664~ - . 4.8640506"'03Y"nCT 27031

Z"'OCT 0616E 2.0446628+0 3C Z"'OCT ~J~02

T. O~PO~ .1'7 8 22J4CT 1220C

40

TABLE VI.- 1M NAVIGATION UPDATES

(a) DOl maneuver

1- 77~UO - .... 997l~b1+lJoX '12110

Y 77613 -3.1 "U'I1 btHUbY 7'1OU1

i. 7771'1 -1.JI;90 ...... ~+UbL !:d ;)~U

X-DOT 66bJJ -J.U11J978+uJX-DOT '1J70~

V-ooT 1'1370 .... U96JbJl+UJY-uOT 267 .. 7

~,. _._. _.- -

Z-uUT 05020 1.bb091.l7+UJZ-UUT 1J 77'"

T O",~U7 99 .l1 ~8.I;UT 12J!)O

41

TABLE VI.- LM NAVIGATION UPDATES - Continued

(b) Phasing

x.- ------ +----------

y

y

U0320 S.~90~28b+UoIi 0 g 6!i ------ --_.._-.. ----- ----- --_.--.

--17 7-2-1--- -----} .. -2 b 3-0 3-'H ... (J 653310

i 77700 -~.2082S2~+O~.-..-.-- -. --2 ..- -----------------~.~-- -.-------- --------- --- --.. -._--

X-LJorX-DOT,

V-DOT.. ------- --¥.~------

I-I)-OT·Z-DOT

-J ~lJ~oSS6!)

b001S

'617~

--1-1"'~1--

'i7023

-}.252J07'i+U3

-Lt.99&+S052+U",._------------_.

T--_ ..,---,.+----

O~2'il lOU 3&+ 20.89·-----,f-,IJ~Otf_i_l,2----_.-.. -.---- ---....---.----- ..- ..-------

42

TABLE VI.- 1M NAVIGATION UPDATES - Continued

(c) Insertion

X 00317 !:J. ~876j2b+lib3~6i5

.. --...

X

V 00077 1.7U80111+UbV 21464

Z 00036 8.122836,++U5Z 0·7100 ..

X-')JT 04355 1.46464-6:)+03X-JUT 2611~

V-JOT ~0623 -4-.9909998+03Y-)JT 45225-

. .._--.- .._-- . - . - -- .

Z-I')JT 71575 -2.u518125+037-)OT 77S47

T O~314 1u2 31 17.30T 254-b~

. -- ~. ----- _... ._--


(d) CSI maneuver

- it • 8 7 1 2. 'f 'I 2 + U6x..._-_._-_ .... ~-_.- -_._.

77512-.---~7.u.C+l-i.-;l-=!:)~------..--..--...--.-.---

yY

X... DOT>'-110T

7771'f.-bl-o-2~.--·..

. 6~.377 .SJ03'i

-,j.!09001'++l/6

-1.J8263a9+U6

-:;. 1-1 } 2. 173 +{j 3

Y-DOT- ¥-I)..Q..l- .---.--.

1~2'f'f ~.O'f2.b8'+2+0J

J §it ~.J..1--_._. __..... -.- ... -.----.-...

Z... OOTL-I)OT

T.• _ •. o· ._I--,,-- ......

"--_._._.. -- ... _....._-_ ...._--

O~337

----ll!i 7 S 11

}ee270"+9'i+1I3

lOJ 21 L16.lIO

44


(e) CDH maneuver

A 0026~ 't • 13 7 1 7!;) 7 b + 1I b.~ 1..Q..l.,}-J- ._--_ ... - -----

y UfJlb'i J.l'i026S3 ... n6y 32102

l UOiJ6J i.J957127+U6L 35012·

X-JOT 1 1J~b J.IUSllU9+(J3;~ - ) Ot- 31251

Y-lid T 63"126 - '•• 0 8 6 6 7 18 + UJV-dOl ~6~Gl--·-- -- --- ._--- .- -"-"-----'

l-·)OT 721b7 -1.6'1S07"11+U3L-'}IJl 71"173

'T UIt J 6 '1 10'. 19 Lj 2 • '10T L17 J+U

45

TABLE VI.- 1M NAVIGATION UPDATES - Concluded

(r) TPI maneuver

X OOU'fJ 9,61StH29+11SX ~070'f

Y 77lt65 -S,'tJ .. 7SJ2+0c,y 7 1175

l 77bS'f -2,2'f58622+U6Z S60 II

X-lJOT S1617 -S,J21lf6S2+0JX-DOl 5»627S

y-OOT 7S~ZO -7, ~&"'O~d7+02Y-OOT 730Jl

Z.OOT 76~66 -",161'+191+U2Z-OOT 02'11"

T 0"1102 10 ... S6 S9,"0.T 0066 ..

TABL

EV

II.-

DET

AIL

EDM

JV1E

UVER

TABL

ES

(al

Ev

asi

ve

man

euv

er

CST

AI"

LsT

A10

STA

Ir'

'viT

94

575.

6[')

....C

gET

V0

C.0

GE:T

V0

0.f

)GF

TV0

0•n

wL---

.-.

CD~

RH

EART~

G[T

RCl

0.0

'WF

•on

GEt

I4

28

47

.6~t

Ba

2.2

DTtg

0.59

REFs

"'IM

AT

DEL

P,9

1FE

r21

174

7,6

I",0

0;0,

V4.

13I'l

lRE

FDE

LV

~,23

DVM

19

,7ve

x"4

,9OR

18

C.7

YR.0

v!-I

3.0

+:-

CVRF~

.0Ve

V-.

6IP

25

4.4

pB,n

PH2

83

,R0

'\

DVC

15

.5VG

Z1

9'1

MV

359

'1RA

,°~H

177

,1

VF5

09H

811~65b,0

HA300ii~::~6

VP.0

0VS

~:co

pH

I3

13

bN

HPTH

ETA

P.0

0

VD1

9,0

1L

131

114

9W

L-AN

0o

ED

ELTA

P~OO

D~

~2('1103,4~

F61

13

1.6

9E

.91

68

16

96

PLL

S0

0N

PHAS~

.DOO

1~1.6128

LLL

Sa

oE

PInIA

SD~T

,00

0a

\liP3

1F

\.5

30

5R

LLS

•00

0~EDr.E

At\'G

000

\.,t\T

n.VD

.tooo

TARG

!;TS

PGN~

AG¥

EXT

ev

cSM

EX[IV

LAM

BERT

MVR

GETI

428

47

.6G

ET

I0

0•u

GE:T

l0

0.0

GET

!0

0.0

VY.

!:,O

949

IIX,0

00

0'!'

F0

0•n

APS

lS0

Vv"'

.00

00

Vy

,.ooo

ux

,00

EL

V.0

0vz

19

.01

44

VZ,0

00

0V

,00

TI'l

0a

.0Z

.00

DTa

,'1

C.0

00

OPT

ION

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Con

tinu

ed

(b)

MC

C-l

man

euve

r

CS

TAID

l.sT

A10

STA

IDW

T9

45

75

,60

weGE

TV0

0,0

GEoT

Va

°to

GET

V0

°,0

WLCO

DpRE

FEA

RTH

GE'T

R0

a,0

WF

,00

GET

!9

384

6,4

Dr

80

,.5

°TTO

.59

REFs

MM

Ar

DEL

p,9

1P

ET

t26

274\

6,4

OT\.

,00

rWTO

4.14

01R

EF

DEL

V_

,2:3

DVM

57

,0VG

X-,6

OR7.

:3YB

.0YH

16

7,2

+-

eVRE

tv'.0

VcY

11

.8IP

92

,0PB

,0PH

31

,9--.

.JD

VC

53.9

VGz

·55

.7M

y1

1.4

Re,0

RH1.

80

,6

VF,,

42

90

H81

477

05,4

HA~0f\667

.71

5VF

',0

0VS

10

:47

pBI

2924

NHP

",5

.10

1TH

ETA

P,0

0VD

..:5

5

TABL

EV

II.-

DET

AIL

EDMfu~EUVER

TABL

ES-

Co

nti

nu

ed

(c)

LO

I-1

man

euve

r

CST

A1C

LsT

AID

STA

Ie!

WT

91

'42

8'0

0we

GE-T

V0

0,

[1G

lTV

n0

,0GF

-TV

00

,0W

L.-

COD~

RtF

LUN

Ar.'

GETR

()0

,nW

F,o

n

GET

I75

454

3,2

CT

B6

1.0

nTTO

.59

REFs

tviM

ATDE

L~

,96

FET

Y9

234

'13,

2[,;

Tl,..

,00

nVTO

5.66

LAN

DIN

DEL

..,2

5DV

M2

97

8,4

VGX

"1~27,7

OR~55,6

YR,0

YH1

92

,/\

~

CVRF

t",

0V

f...

e9

4,o

IP2

26

,5pB

,0

=~If

'.?

())

DV

C2

97

2.2

VZ

2c86

,9M

y3

41

,7R

8,

01

80

'2

VF"'

27

48

01H

817

7,7

HA1

71

,29

6VP

,00

VS..5

87

;45

p81

141

5HP

52

,09

0TH

EtA

P,0

0Vo

"'98

6,8

7L

HI

16=

33

WL.

liN1

79

36W

DF'L

TAP

35

9,1

0CH

"'9

9),

83

FH

I~43'18

I:.'0

56

84

46

1P

LLS

00

N

PHA

SE,0

00

I1

78

,70

21

LLL

S0

0E

FI-1

AcE

DC'!T

,00

0a

wp

"7

,10

44

RLL

S9

)/\,

49

3Io

EDGE

A~G

,00

0L;~TIL

YO'0

00

0TA

RGET

S

FGN~

AGS

EXT

C;V

C!'M

EXT

evLA

MBE

RTM

VRG

ET!

7fi)

454

3,2

GET

!0

a,u

GfT

I0

0.0

GET

!0

a.0

VY..

.29

H,9

t98

'IX,0

00

0T

F0

0,0

ApS

IS0

Vv"5~7,4500

VV,0

00

0)(

,00

ELEV

.00

V7"2

00

,97

00

liZ,0

00

0Y

.00

TPI

00

,0z

.00

DT0

•nc

.non

OPT

ION

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(d)

~OI-2

man

euve

r

CST

/lIn

GE

TV0

0CO

DE

I.sT

A!D

GETV

00

,nRE

FLU

NAR

STA

ID

GE'T'

V0

0Gr

eTR

00

,0 .0

WT

We:

WL WF

68

86

7.1

5

OCT

A~'G

TARG

ETS

GE

T!

PE

TI

CVM

DV

R!:f

"DV

C

vF vs VD r,H PHA

SEPH

ASE

~EDr;E

vr,

HO

10

45

.59t

'JC;

94

5.5

138.

5 ,01

32

.3

-l3[1,~O

.0(l

-,Y

l-9

Q6

,40

.00

0.0

0

,6888

Di

e0

13

,6DT

L.20

,OU

Vc;X

-10

8.0

VG

'f.0

VC;Z

H6,

7

folB

t5

1.9

PB

IC

17N

LB

11

64

2E

FB

I:!

59

,68

olJ

li~TtL

DT r"VOR IP MV HA HP L.

ANE I w

p

TO,5

9TO

5,8

2

219:

~3

59

.7

58

,61

9~7,900

176

41E

,00

03

60

66

1?f

1,7

59

87

,90

68

RE

FS

MM

AT

LAN

D!N

VB

.0pa

,0R

B,0

vP TI-lE

TA

PD

E:L

TAP

PLL

sL

LLs

RLL

S

DEL

PDE

LV

Viol PH RH

,00

,DO

35

9,0

4a

0N

on

E9

38

,49

3

1..

....

.6

6

18

0.'

35

9.'

18

0.0

Fr.

NS

PT

f,V

(jE

T!

V~ V..,

V7

csn

110

104

5.5

-13

8,~ocn

'CO

C!"

!,C

DC

"

AGS

EXT

CVG

ETI VX Vv VL

oo

.0,0

00

0'0

080

,00

0

GE

TI

TF X V Z C

LA~1BERT

o0

o0

.0 ,0 ,oci 00 :00

.00

0

MVR

GET

!A

pS!S

ELEV

TP! nT

OPT

ION

o o

a,0

a,a

do

0o

:0

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(e)

Sep

ara

tio

nfr

omLM

c.~

TP.

JL.

~5

';'

jl,

;::>

TA1

"1\

I36

484.

00l'

L("

t.r

\u

lJ.u

\:II:.

I"

Uu

.L("

t.I

vu

..J.u

h~

,"<

Ju

t.tl

i;.f

L.U

f.A

tII>

t.rt<

\wu

.uil

f

GU

19

&"L

.I!:

I'CO

!.iT

bu

6.4

LJr

Tu

.OU

r<!:.

f:;

'MM

AT

LJt.L

f'0

.00

..l_

PlT

JII

!:>i.

"IS

.b

.,Tu

.ULJ

uvT

u.O

UL.

AI\L

JIN

ut.L

.Y

0.0

0li

vMi.

.!:1

VI"

A-~.'i

UK

JoL

J.u

YI,)

.wYH

IdU

.WU

vk

tM.u

v(;,y

.lJ

1fo'

19

'i.U

Pc

·uPH

"Il

l.,)

Dv<

J".

!:I

VI"

L•

bM

Y.U

Kd

.wI'C

HId

u.U

IJf

-.L

JIH

b1

~7'9

HAb

U.J

7]

VI'

.OU

v~

.LlI

..I:)

ILJ

!:I7

f',11

t'~9ol;7

TH

t.IA

P.O

U\J

1 0V

U2.

!:>u

LI:

)1

39

8E

L.AI~

11

7't!:

>E

Dt.L

.IAP

J~9.0't

-99

b.J

!:>

FJ'

i'i

011

'-.

LJU

Uco

u"

1-9

--llH

d1

t.f'

L.L.

S0

U1'4

f'HA

St.

.l,;U

LJ1

17

Ci.

/o"'

tL.

L.LS

uU

EPhA~t.

(jUT

.Uu

l,;0

Iif'

I'H

.IJJJ

kL.

LS9

Jd

.'t9

3I,

t."

,,!:.

A/II

G.U

UU

Ut'.

TIL

.Y

u.u

uU

U

P(;

,NS

lXf

llv

(;,1

;.l1 vii vY 'II.

CS

M

9Ci

J!:>

15

.6.L

JUU

u.L

JOLJ

Ui..

!:IO

LJU

AbS

EII

ID

V(;

,£T

IvX v

YV

Z

uo

.U.u

uuu

.OO

Uu

.UU

UU

bt.

TI

T~ >.. y I. (.

.0 .Ll

.UI,

)

.UU

.uu

.uu

u

MV~

(;,I;.

Tl

AP~IS

t.L.t.

vT

pl

UTu

pT

IUN

o u

u.U

U.L

lUU

.Uu

.u

o/t

lbb

.9J

f'T

klM

.uu

.uU

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(f)

DO

lm

aneu

ver

CST

AID

GU

YC

OO

Eo

0.0

LST

A10

l:aE

TVR

Ef

o0

.0L

uN

AR

Wi

Jr~D2.cro-

weu

iJ.0

WL

-----~

-

uu

.0w

f.0

0

CJI:.

T199

J3sa

.a0

1-8

1)-

26

.9II

IT

O-

--

0.3

8R

EFSM~~T

--

D~L

.p.

&.'

fl-

PE

TI

11

62

25

8.8

LIT

U8

.00

i,lV

TU2

.38

_LA

NO

Itil

DEL

.Y

!:I.

39U~M

71•

1V

GX

1y

•1

OYJb

U.l

IV

b.u

-'o

r-

17

9.,,--

-

DV

RE

M.0

VbY

.0IP

28

b.l

Pa

lBb

'lPH

3!:1

9.9

\Jl

----

---

69

.6------'{~---

68

.5-rfI(

.b

---R

a---

••RH

~tiO.o

.-..DV

C

DO

Tli

NG

VF VS VO

OH PH

-A-S

EPH

ASE

wED

GE

YO

-71

.1U

.00

-.'

i9 .uo

.00

0.0

00

0.0

00

.00

.oou

u

H6

1p

dl

L.1)

1f

dl

~l~.-HA

~9.'i'O

ypl~Oo

osa

5H

P8

.78

6T

hET

AP

.OU

13

9"5

,.i.

.AN

PIS

JE

·OELT~

P--

3S

9.0

1t

IS9

.U7

~.U

26

08

95

9P

LL.S

00

N------1

-----

---r

fij--

;7b2

-J--

-L--CL~------

--·6

--U

--C

----

---

o0

WP

12

8.7

38

9R

~LS

93

8.'

t93

UN

TIL

.

TAto

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(g)

Ph

asin

g

CST

A11

,1L.

ST

Alu

SIl

l11

,1I'd

JIU

b'f

.9L

J11

(.

C:a

EHU

U.U

C:aE.

TVu

U.1

IC:a

t.TV

UU

.0i'l

L.

tou

EkE

FL.

UN

At<

C:aI:

.Tk

u1.1

.0I'

tf

Gt.

TI

lUU

'to

20

.9liT

6U

Ii1

.7In

TO.3

bt<

EfSM

MA

TlJE

L.P

!;).

't7

PU

I1

17

35

2U

.9I.>

TU

8.0

Uu~

TUl.

'tJ

L.A

I'4U

INOI

:.L.

Y5

.39

OVM

19

5.4

VGJl.

-2U

.8UY

30

0.U

YI;

·uYH

.7

I)VRE

M.0

VeaY

.0IP

lb't

.'+

Pb

20

't.'

tPH

2'1

.3

DVC

19

3.0

Veal

.1

9'1

.3M

R.0

RB.6

RH.J

VF1

71

.28

H1;

11

5,.

3HA

19

0.9

,+2

VP

-,6

1

VS

-.0

0P

bl

01

NH

P7.~'t9

TH

t:TA

P.O

UVD

-9,+

.U2

L1;

111

1't

WL.

AN1

16

~2

EO

EL.T

AP

.3!;

)9.U

't

UH0

.00

fI;

1,+

8.'

t6E

,UlU

36

1tl

iP

LL.S

(IU

N

PHA

SE.

00

0.0

00

Il1

a.7

6l1

L.L.

L.5

UlJ

E.PH

ASE

OU

T0

.00

00

ilIP

-2il

tt.J

.:!:

»:a

RL.

L.&

9.3

6.'

+9

3III

EOG

EAN

l.J,O

OU

urH

ILYI

.>,u

ouu

\J1 I\)

PCloN

SA

eas

EXT

ovL.M

!:.X

lDV

LAM

bEl'I

1MV~

HT

l1

00

't6

20

.9II

t.T

IIO

U't

62

U.9

<aU

IU

1.1.U

TABL

EV

II.-

DET

AIL

EDMANEu~R

TABL

ES-

Co

nti

nu

ed

(h)

Inse

rtio

nm

aneu

ver

--_

._-._

-._

-------------_

.__•..........

__.

-..

_---

CST

AID

~sJ\L_

CODE

LST

AID

STA

Ii)

.0 ~o

IfJT

84

20

.80

we wL--

iJF

'..-

---.

----

.00

-·

GE

T!

PE

TI

----

~>-I

,.'~

~-_.

D

VRE"

1DV

C

10

24

31

7."

\1

19

32

17

.92

07

.0 .02

05

.8

DT

A0

15

.0D

TTO

.10

REF

SMM

AT

JEL

P.0

0D

TU

~.oo

~v

TO1

.17

[AN~IN

~EL

Y.0

0V

GX

96

.8OY

18

0.0

YB

.0YH

16

0.0

VG-:-:

--Y--

---~1---ip-·--··--62.-

1--

·PS

---=

2:- li

-i:1-

---

P-H

·---

--2ij·~-~------

VGZ

-18

2.9

~R

.0RB

18

0.0

RH3

60

.0

VF VS VD -:5

tr.

PHA

SEPH

ASE

wEDG

EYD

-18

8.5

5H

318

.0H

A4~.~6~

vP.1

0P

310

39N

HP

6.~57

THET

AP

-85

.36

L31

19

0E

~AN

17

62

2E

DEL

TAP

0.0

0·-·nI----35-~f2--

--I-

-.0

1-92

lJ74

2--

·F'-

iLS

00

0.0

00

11

78

.76

3£

+~

LL

SJO

T0

.00

00

"P1

28

.14

3(j

RL

LS

~NG

.00

1U

NT

IL.o

oon

TA

RG

ET

S--

----

----

----

----

-_._

----

-.9

3.0

03

59

.04

tJ·--

-O--

N--

->--

----

----

.

o0

E9

38

.49

3

PGN

SEX

TJV

GE

T!

VX VY Vl

l,\·1

10

24.

317.~

-18

9.2

00

0.1

00

n-8

5:90

00

AGS

EXT

JVG

ET

!VX VY -V

-i.-

10

24

31

7.b

-1~8.20bb

.10

00

~13-6

~To-;3

GE

T!

TF X Y Z C

L.A

,"1S:

:RT

o0

o0

.0 .0.0

0.0

0.0

0.0

uO

~VR

GE

T!

APS

ISE

LE

V--

tPI

iHJP

TIO

N

o o

o.0

o .0

00

--.0

---

o.0

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(i)

CSI

man

euve

r

::,r"

1D

L::,

1"

1c'

t,l/

,[

:J',I.

fil

2'1

2'

IIlJ

wef,

Cr

v'J

0.0

r~l

T~

U0

.tJ

(,t:.

r\0

U.0

',\L

~

rilD

[PC

t:FL

UH

;-.H

(,E

rf-

0a

.0w

F

[Ii:

.1

[j

0J

33

"tA

.1)

()I

[\0

);~

•3

DT

TO.0

0R

t.fS

MM

IIl

p.~

rI

i2

JL

2'i6

.(j

lJT

lJ.u

o0

'1TO

.ou

L""

"OIN

l'V

M50

.5\

\,x

-IJ.8

uy•

(1YB

.0O~h:t.11

.0V

(.'(

--

..0

!P1

0S

.il'

-p

a--

Ifr

n-t

lDV

C<

,lJ

•!:>

'v(,

I-'1

8.6

~1H

.lb

U.U

~~

36

0.0

[JE

LP

OEL

YH

IP

+t

Rtt

.ou

.UD

36

0.0

35

9.9

36

U.U

\J1 +-

!:>

L.':

>n

ht<

I\'

:".O

Ufo'

tl1

I,I

•1

.lL

!.l

tn,

0·0

0;

-,b

-l--

".,f

,St.

00

0.0

00

~',11\

':iE

!,H

J!0

.00

;r,l

lG

tA

ft(,

•(I

00

vq

.OO

OU

'13

.1o

Sk

51

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TAB

LES

-C

on

tin

ued

(j)

CDR

man

euve

r 5T

A10

C':>T

Al

[I

(iL

lV

_._

,UJJ

l£

LST

A1

0

U0

.0~~TV

0.

._

.._

_H

£.L

......

o.0

II/

(~

IIl~

NT wea

0.0

WL

'--40~·--<QIf-----..

i}----M

--

-

81

96

.90

\J1

\J1

REF

SMM

AT

OEL

P.0

0.

lA

Hi)

JN

0E

LV

.Oi)

--

VB

.0V

II1

80

.0--

P-B

--"-

'-.zri-

-p

tt---

·Z1

t.'t

·.-]

--RB

18

0.0

~H

36

0.0

.0

TO•

00

TO.O

Gla

o.n

18

20

,3-·

-

(iL

T1

10'1

31...

2..

..DT

80

2.2

DT

f'I~

TI

12

JL

a'1

2.'1

ur

u.0

0.o

vilV

I13

.4v

(il\

-3.'

1O

YU

IHEM

.·.u

._1

l4-¥

-__

._---..i}

.--1~'

.'-'.

DVC

j.'I

II(,

L•

IM

H

VI'

'J';j

'JI)

llii

!'d

AS

EP

HA

SE

IIU

JGE

'(IJ

DO

TA

NG

·.S

OIi

til

.no

~B

I:\

•.3

0L

f1I

....U

J..L

..___

_L.

tH0

00

.00

00

.00

.uoo

.QO

OO

"'2

.8IJ

~8

N3

73

0E

1'1

.98

a0

UN

TIL

rlA

'15

.12

9li

PH

P~~.ld6

TH

ET

AP

LAN

17

9~s

ED

EL

TA

P_

.---

f.-_

.-_~'u:w

7-1

--··

P~:i-

I1

78

.76

35

LL

LS

.r188.~133

RL

LS

-1.0

0.e

o3

S'l

.0'l

··-9

-·-0

.~-_.

OD

E9

38

.'1

93

Tf\~GETS

LM

IBE

IHlJ

08

-0

"'"

J5L

AI

Dv

(;t:

rI vx Vy

..vL

L/1

10

'1-3

1'1

2.'1

-.8

0U

O.o

uoo

3.3

00

0

.,c,

SI.

AT

all

(;I:

.Tl

lU'l

vj(

--

VY ....L

..-

.._..

..

31'1

2.'1

GE

TI

-.8U.~2

TF

.00

00

X'-

J..

29

9J..

..-

--_

..v. l c

.0 .0.0

0-------.-

GO

··-

.00

.00

0

HV

RG

ET

Ia

AP

SIS

EL

Ev

-H>

-l--

-"-

._{}

DTO

PT

ION

o.u

o.0

0..

0---.

fr_

·--

a•u

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Co

nti

nu

ed

(k)

TPI

man

euve

r

CST

A1

0L

ST

AIU

STA

ID\'iT

819

)'7

°we

GETV

00

.0G

ETV

a0

.0G

ETV

0a

.0i'l

L

COD

Efo

TABL

EV

II.-

DET

AIL

EDM

ANEU

VER

TABL

ES-

Con

clud

ed

(1)

TE

lm

aneu

ver

------~-

STA

10C

5TA

ID

---;

6T

'L_

---

JL.~

.1'

.i.I

V.

O__.

.Q.J

l._.

__#

IYCO

DE'

REF

L.UNA

RGE

TR

WT

'66

65

.79

.We

1.0..

---_.

Wl.

----

----

--.-

---

.0W

F

GE:

TI1;

:$72C~2."

Dr

E!~

48

.5.

DT

fO.5

9R

EFSM

MA

TD

ELP

"'.'2

PETI

1'4

9~2.4

OT~

20

,00

0'1TO

15

.20

LAN

D!N

eEL

Y.2

3C

VM

--..

~t2.2..7

--.

VG

X--

--2

i22

..L--

--.!

1.R

----

-1'.

-9.9

...:

..--

-.v

s---

---

··..-..

.0-

."tJ

oi-

----

----

..A

---

CVRE~

.0V

GV

-)4

,3IP

51

,3Fe

.0PH

34

9.2

DVC

3607

.0VG

z_1

I-29 J

.5.t

7_

_M

y..6

Ra

.n

RH.

179.

6....

.

VF VS \l0

-_DH PH

ASE

PHA

SEwE

DGE

YO

OCT

ANG

H81

57.0

p81

C&

S1.

et--15~_JJ

-E-

"B

I1

1,6

8

oa

LJt\T

1L.

.TA

RG

E1S

PGN

SEX

TDV

GET

IV

'A. Vv Y'l.

cSM

1;5'7

202

2.4

36

18

.06

62

":3.

4175

241

76

44

9'

,

AGS

EXT

CVG

ETI yX y~ VZ

a0

,0,0

00

0

-:8~g

GF-T

IT

F -x V z e

L.AM

BERT

o0

o0

MIIR

.0G

ET

l,0

APS~S

.8g-

---;

~1v

:00

oT.0

01'.1

OPT

ION

a0

.0o

-·-

----

1-00

a0

.0o

.0

58

TABLE VIII.- FDAI ANGLES FOR LM MANEUVERS

Maneuver Roll Pitch Yaw

DOI 0.600 286.100 -0.

Phasing 0.600 264.400 -0.

Insertion 180.000 242.100 360.000

eSI o. 105.800 -0.

eDH 180.000 2.300 360.000

TPI 0.240 196.689 0.120

TABL

EIX

.-CS

MEX

TERN

AL

~V

UPD

ATE

S

(a)

Ev

asiv

em

aneu

ver

01

0FC

TD

SKY

V71

DE

CIM

AL

1IN

DE

X

2A

DD

3V

GX

00

00

10

.50

94

90

00

E0

1V

1

4V

GX

37

46

7\0

5V

GY

00

00

0O

.

6V

GY

00

00

0

7V

GZ

00

00

70

.19

01

43

99

E0

2

10

VG

Z1

53

06

11

TIG

N0

01

42

42

84

7.5

6

12

TIG

N1

57

24

TABL

EIX

.-CS

MEX

TERN

AL

6VU

PDA

TES

-C

on

tin

ued

(b)

MC

C-l

man

euv

er

OlD

FCT

DSK

YV

71D

ECIM

AL

1IN

DEX

2AD

D

3VG

X7

77

57

-0.4

29

02

24

6E

02

4VG

X5

03

03

0\

0

5VG

Y0

00

04

0.1

04

65

28

7E

02

6VG

Y0

25

17

7V

GZ

77

76

1-0

.35

99

20

11

E0

2

10

VG

l7

65

16

11

TIG

N0

03

23

93

84

6.3

8

12

TIG

N3

63

76

TABL

EIX

.-CS

MEX

TERN

AL

~V

UPD

ATE

S-

Co

nti

nu

ed

(c)

LO

I-1

man

euve

r

OlD

FCT

DSK

YV

71D

EC

IMA

L

1IN

DE

X

2A

DD

3V

GX

75

61

7-0

.29

12

91

98

E0

40

\

4V

GX

61

25

4f-

'

5V

GY

77

43

2-0

.58

74

49

98

E0

3

6V

GY

71

72

5

7V

Gl

77

66

1-0

.20

09

70

03

E0

3

10

VG

l6

27

57

11T

lGN

03

20

07

54

54

3.1

7

12

TIG

N2

61

15

TABL

EIX

.-CS

MEX

TERN

AL

~v

UPD

ATE

S-

Co

nti

nu

ed

(d)

LO

I-2

man

euv

er

OlD

FCT

DSK

YV

7l

DE

CIM

AL

1IN

DE

X

2AD

D

3VG

X7

77

11

-0.1

38

49

99

9E

03

0'-

4VG

X7

67

03

(\)

5VG

Y0

00

00

o.

6VG

Y0

00

00

7VG

Z0

00

00

O.

10VG

Z0

00

00

11T

IGN

03

34

180

104

5.5

2

12T

IGN

30

05

0

TABL

EIX

.-CS

MEX

TERN

AL

~V

UPD

ATE

S-

Co

nti

nu

ed

(e)

Sep

arat

ion

from

LM

'01

0FC

TD

SKY

V71

DE

CIM

AL

1IN

DE

X

2AD

D

3V

GX

00

00

0O

.

4V

GX

00

00

00

\W

5V

GY

00

00

0o.

6V

GY

00

00

0

7V

GZ

00

00

00

.25

00

00

00

E0

1

10

VG

Z3

71

54

11

TIG

N0

41

66

98

35

15

.60

12

TIG

N0

73

50

TABL

EIX

.-CS

MEX

TERN

AL

6VU

PDA

TES

-C

oncl

uded

(1')

TE

lm

an

eu

ver

01

0Fe

rD

SK

YV

71D

EC

IMA

L

1IN

DE

X

2A

DD

3V

GX

02

60

30

.36

18

06

62

E0

40

\

4V

GX

22

10

7+:

-

5V

GY

77

76

2-0

.34

75

24

18

E0

2

6V

GY

56

10

1

7V

Gl

00

10

40

.17

64

49

70

E0

3

10

VG

l3

27

20

11T

IGN

05

71

11

37

20

22

.41

12

TIG

N2

67

00

TAB

LEX

.-LM

EXTE

RN

AL

t:::.V

UPD

AT

ES

(a)

DO

rm

aneu

ver

OlD

FCT

DSK

YV

71D

EC

IMA

L

1IN

DE

X

2A

DD

3VG

X7

77

44

-0.7

10

99

99

7E

02

~

4VG

X5

02

57

V1

5VG

Y0

00

00

O.

6V

lJY0

00

00

7V

GZ

77

77

7-0

.27

00

00

00

E0

0

10

VG

Z7

45

01

11T

IGN

04

21

39

93

35

8.8

0

12

TIG

N2

74

50

TABL

EX

.-LM

EXTE

RNA

L~v

UPD

ATE

S-

Co

nti

nu

ed

(b)

Ph

asi

ng

man

euv

er

01

0F

Cr

DSK

YV

71D

EC

IMA

L

1IN

DEX

2A

DD

3V

GX

00

10

20

.17

04

00

00

E0

30

'\

4V

GX

17

30

10

'\

5V

GY

00

00

0O

.

6V

GY

00

00

0

7V

GZ

77

73

2-0

.95

59

99

96

E0

2

10

VG

L6

63

60

11T

IGN

04

24

61

00

46

20

.89

12

TIG

N0

75

10

TA

BL

EX

.-LM

EXTE

RN

AL

/',.V

UPD

AT

ES

-C

on

tin

ued

(c)

Inse

rtio

nm

aneu

ver

OlD

FeT

DSK

YV

71D

EC

IMA

L

1IN

DEX

2A

DD

3V

GX

77

66

6-0

.18

91

99

99

E0

3

0'\

4V

GX

45

72

2--.

.:l

5VG

Y0

00

00

0.9

99

98

00

0E

-Ol

6V

GY

01

17

7

7V

GZ

77

73

7-0

.83

89

99

94

E0

2

10

VG

Z5

04

24

11T

IGN

04

32

11

02

43

17

.80

12

TIG

N0

21

04

TABL

EX

.-LM

EXTE

RNA

L~V

UPD

ATE

S-

Co

nti

nu

ed

(d)

CSI

man

euve

r

DID

FC

rD

SKY

V71

DE

CIM

AL

1IN

DE

X

2A

DD

3V

GX

00

02

30

.50

50

00

00

E0

2

0\

4V

GX

26

36

2co

5V

GY

00

00

0O

.

6V

GY

00

00

0

7V

Gl

77

77

7-0

.60

00

00

00

E0

0

10

VG

l7

04

04

11

TIG

N0

43

43

10

33

34

6.0

0

12

TIG

N2

14

50

TABL

EX

.-1M

EXTE

RNA

L~V

UPD

ATE

S-

Co

nti

nu

ed

(e)

CDR

man

euve

r

01

0FC

TD

SKY

V71

DE

CIM

AL

1IN

DE

X

2A

DD

3V

GX

77

77

7-O

.SO

OO

OO

OO

E0

0

4V

GX

-06

00

5(j\

\0

5V

GY

00

00

0o.

6V

GY

00

00

0

7V

GZ

00

00

10

.33

00

00

00

E0

1

10

VG

Z1

11

46

11

TIG

N0

43

70

10

431

42

.40

12

TIG

N3

04

40

TABL

EX

.-LM

EXTE

RNA

L~V

UPD

ATE

S-

Con

clud

ed

(r)

TPI

man

euve

r

OlD

FeT

DSK

YV

71D

ECIM

AL

1IN

DEX

2A

DD

3VG

X0

00

10

0.2

20

99

99

9E

02

4V

GX

23

72

2-.

J0

5VG

Y0

00

00

0.0

99

99

99

9E

00

6VG

Y0

11

77

7V

Gl

77

77

3-0

.11

30

00

00

E0

2

10

VG

l6

27

30

11T

IGN

04

40

61

05

85

9.4

0

12T

IGN

15

36

4

71

TABLE XI. - MANEUVER PADS


P30 MANEUVER-

PURPOSE

SET STARS S p s /C & N PROP/GUID

9 4 5 7 5 .6 WT N47

R ALIGN + 0 0 0 9 1 PTR1M N48- - -P ALlGN_ + 0 0 0 2 3

YTR1M- -

Y AlIGN_ + 0 0 0 0 4 HRS GETI--+ 0 0 0 2 8 MIN N33+ 0 4 7 5 6 SEC

ULLAGE No ullage + 0 0 0 5 1 I'NX N81

+ 0 0 0 0 0 I'Ny+ 0 0 1 9 0 "N Z

8-

X X X 1 1 R

X X X 2 5 4 P--- --

X X X 3 5 9 YHA

-+ N44

+ 1 1 9 4 Hp (DMT)

+ 0 0 1 9 7 6VT

HORIZONjWlNDOW _ X X X 0 0 3 BT

X 0 0 1 5 5 6VC-

X X X X 2 4 SXTS

+ 2 7 3 3 0 SFT

+ 0 8 2 0 0 TRN

X X X BSS

X X SPA

X X X SXP

OTHER 0 LAT N61

LONG-t RTGO EMS

+ V10

I GET O.OSG

72

TABLE XI.- MANEUVER PADS - Continued

(b) MCC-l

P30 MANEUVER

PURPOSE

SET STARS C' p s VG & N PROP/GUID,j

9 4 5 7 5 .6 WT N47

RAl.IGN + 0 0 0 9 1 PTR1M N48- - -P ALlGN_ + 0 0 0 2 3

YTR1M

- -y ALlGN_ + 0 0 0 0 9 HRS' GETI- -

+ 0 0 0 3 8 MIN N33+ 0 4 6 3 8 SEC

ULLAGE No ullage - 0 0 4 2 9 f:N X N81

+ 0 0 1 0 ,-f',.Vy---------- )

- 0 0 3 6 0f',.V z

X X X 0 0 7 R

X X X 0 9 2 P

X X X 0 1 1 Y

+ HA N44

- 0 0 0 5 J Hp (m1T)+ 0 0 5 7 0 L\VT

HOI IZONj'NINDOW _ X X X 0 0 8 BT

X 0 0 5 3 9 f',.VC

X X X X 1 6 SXTS

+ 0 9 9 5 0 SFT

+ 2 4 6 0 0 TRNX X X BSS

X X SPA

X X X SXP

OTHER 0 LAT N61. ~- f--

LONG+ RTGO EMS

+ VIO

I GET O.OSG

73


(c) LOI-l

P30 MANEUVER

PURPOSE

SET STARS S P S /G & N PROP/GUID

+ 9 2 4 2 8 WT N47

R ALIGN + 0 0 0 9 6 PTR1M N48- - - YTR1MP ALlGN_ - 0 0 0 2 5- -

Y ALlGN_ + 0 0 0 7 5 HRS GETI--+ 0 0 0 4 5 MIN N33+ 0 4 3 1 7 SEC

ULLAGE No ullage - 2 9 1 2 9tN

X N81

- 0 5 8 7 4 6Vy

- 0 2 0 1 0 6V ZX X X 3 5 6 R

X X X 2 2 8 P

X X X 3 4 2 Y

+ 0 1 7 1 3 HA N44

+ 0 0 5 2 1 Hp (DMT)

+ 2 9 7 7 9 6VT

HORIZON/'NINDOW _ X X X 6 02 BT

X 2 9 7 2 2 6VC

X X X X 2 1 SXTS

+ 2 6 7 5 0 SFT

+ 1 6 0 0 0 TRN

X X X BSS

X X SPA

X X X SXP

OTHER 0 LAT N61

LONG+ RTGO EMS

+ Vl0

I GET O.05G


(d) L01-2

P30 MANEUVER

PURPOSE

SET STARS S P S/G & N PROP/GUID

+ 6 8 8 6 7 WT N47

R ALIGN + 0 0 1 4 4 PTR1M N48- - - ---- YTR1Mp. ALlGN_ - 0 0 0 6 6- -

Y ALIGN_ + 0 0 0 8 0 HRS GET!-- -+ 0 0 0 1 0 MIN N33+ 0 4 5 5 2 SEC

ULLAGE 2 quad - 0 1 3 8 56V

X N81

20 second + 0 0 0 0 0 6Vy

+ 0 0 0 0 0 6V ZX X X 0 0 0 R

X X X 2 1 9 P

X X X 0 0 0 y

+ 0 0 5 8 6 HA N44

+ 0 0 5 7 9 Hp (DMT)+ 0 1 3 8 5 6VT

HORIZON/\VINDOW _ X X X0 1 4 BT

X 0 1 3 2 3 6VC

X X X X 2 2 SXTS

+ 0 1 9 1 0 SFT

+ 0 5 8 0 0 TRN

X X X BSS

X X SPA

X X X SXP

OTHER 0 LAT N61-- -LONG

+ RTGO EMS

+ V1Q

f GET O.OSG

75


(e) Separation from LM

P30 MANEUVER

PURPOSE

SET STARS R C sVG & N PROP/GUID

+ 6 7 8 8 6 WT N47RALIGN + 0 0 0 0 0 PTRIM N48- - - Y

TR1MP ALlGN_ + 0 0 0 0 0- -Y AlIGN_ + 0 0 0 9 8 HRS GETI--

+ 0 0 0 3 5 MIN N33+ 0 1 5 6 2 SEC

ULLAGE RCS only + 0 0 0 0 0 tNX N81

+ 0 0 0 0 0 t:Ny

+ 0 0 0 2 5 t::.V ZX X X 3 5 9 R

X X X 1 9 4 P

X X X 0 0 0 y

+ 0 0 6 0 0 HA N44

+ 0 0 5 9 5 Hp (DMT)

+ 0 0 0 2 5 ~NT

HORIZONj'NINDOW _ X X X 0 0 6 BT

X 0 0 0 2 5 6.VC

X X X X 1 6 SXTS

+ 2 5 8 6 0 SFT+ 1 5 8 0 0 TRN

X X X BSS

X X SPA

X X X SXP

OTHER 0 LAT Nol

LONG+ RTGO EMS

+ Vl0

I GET O.OSG

76


(r) DOr

~~'-r-

+ 0 0-- ----- -~. ~-t 0 0- f---- ~--- -+ 0 ._-

~ f--.

~t~--I-x~H---x ~t;.(-

x x xI

-- I--- -

--- -- --- -'---- '----x X X

- _ . . - P--- .-X X~-xtxf--~__L ___

REMARKS:

-

--_.__._------_._._-------....,...-.--,P30 LM tAANEUVER

N81LOCAL

VERT..-

Ullage: 2 quad, 8 sec

77


(g) Phasing'-

P30 LM MANEUVER

T P H A S I N G1. PURPOSE+ 0 0 + 0 0 1 0 0 HR N33

f--

+ 0 0 0 + 0 0 0 4 6 MIN TIG+ 0 + 0 2 0 9 0 SEC

+ ° 1 7 0 4 t:,.VX N81r----+ ° 0 0 0 0 t:,.VY LOCAL•- ° 0 9 5 6 t:,.VZ VERT

+ + °1 1 9 5 4 t:,.VR--X X X X X X 0 4 2 BT

X X X I X X X 0 0 1 R FOAl.--L-X X X

I

X X X 2 6 4 INERI P1 + 01 1 7 2 0 f::,VX AGS N86

~--- -)--t l + °1 0 0 0 0 tNY AGS-- --I--~---, - .-t7 AGSi ~ - °I 0 9 2 t>VZ1"--- --

X X X I I X xi X N A COP-.S--+--+2-- --e-X X -I· -1· ·X:EI AZ--e-X X : X X 1 EL~

~.-_I-_-

REMARKS:Ullage: 2 quad, 8 sec

78


(h) Insertion~- -----------.------

P30 LM ~IIANEUVER

N81LOCAL

VERT

REMARKS:

Ullage: 2 quad, 4 sec

79


(i) CSI

P32 C51 UPDATE

•

HRTIGMIN

5EC C51

+ 0 0- _._. ,---- .__._- -_.-+ 0 0 0...__ . -,._-- .. -. -..-. ._- '.

+ 0

+ 0 0_." -- --_. - _.+ 0 0 0

... .,.. ,+ 0

+ 0 0 1 0 3+ .. ·0 1 0.0' 3- j-3.. .1 __+ 04;6.0 i O+ 00 1 0 5

• ~ - - ~ --- t --.-

+ 0 0 0 0 8+ 6' 5 9 "4'0•

HR

mNSEC

TIGTPI

Nll

N37

N86l1VX AGS

11 VY AGS

l1VZ AGS

!J. VX LOCAL N8111 VY VERT

PLM FOAl

•

- -,o 0

Io 0-ntil~

o I 0f----_

• 11 VXAVY

6.VZ

AVX

11 VY

l1VZ

N81PGNCS 1----1LOCALVERT

CHARTS N81LOCALVERT

REMARKS:4 quad, +X


(k) TPI

P34 TPI UPDATE

HR TIG N37MINSEC TPI

t,VX N81t,VY LOCALt, VZ VERTt,VRRLM FOAl N42PLM INER

R TPI N54TIG-5

R TPIF/A{+/-} N59R/L{+/-} t,VD/U{+/-} LOSBT

F/A PGNCS N59R/L t,V

DIU LOS

F/A CHARTS N59R/L t,V .....

LOS 0-D/U t-

~

•

•

•

- ~ .

o 0

o 0•

••

•

ONBOARD LOG

+ 0 0 2 4 8..- .....- I-- .. - i -_.

+ 0 0 0 0 1_.'--I--"-~' _....

• - 000 0.1

+ 0 33 ,14• .-.. I-- . ..L ...• •.. _

- 0'1'0 97• •

••

o 0o 0

....... --- t--

o 0

X XX 0' 0 ' 0. . . __.....:..._._.t _

X X X 197

xxxxxxxxxo 0

o 0 .. - ...... . t--o ,0o 0

x X Xo 0

+'Oio' +'O:0!1 1 0 5- -- ~ -- : _. i -1-- ... :-_._; --;- t---- j--'+10,00 +,000 Oi8- '-- .. ----'.-- .. ---- .-----\- ;---1--·_·'·+ 0 i.! + 05'9. 4i O

x X X.- - .. -- .-X X X

. + 0 0

+ 0r--

o

+ 0!o,212;1.- -. +-_. I-- -., ..:..-

+ 0:0 010:1~ .. - ,-'" -: -.~ 0 i'o:1--' i--: 3,~

!x X

o 0o 0

I 0 0

..

r.-----i REMARKS:

4 quad, +X

-82

TABLE Xl.- MANEUVER PADS - Continued

(1) TEl

P30 MANEUVER

PURPOSE

SET STARS S P S I7G & N PROP/GUID

+ 3 6 6 6 6 WT N47RALIGN - 0 0 0 7 2

PTRIM N48- - -P ALlGN_ + 0 0 0 2 3

YTR1M- -y ALlGN_ + 0 0

1 3 7 HRS GElI--+ 0 0 0 2 0 MIN N33+ 0 2 2 4 1 SEC

ULLAGE 2 quads + 0 3 6 1 B.l ~VX N8120 second - 0 0 3 4 8 ~VY

+ 0 1 7 6 4 ~Vz

X X X 1 8 0 R

X X X 0 5 1 P

X X X 0 0 1 Y

+ N A HA N44

+ 0 0 5 9 1 Hp (DMT)

+ 3 6 2 2 7 ~VT

HORIZOt"-l/WINDOW _ X X X 24 9 BT

X 3 6 0 4 8 ~VC

X X X X 1 1 SXTS+ 0 1 4 9 0 SFT

+ 2 1 8 0 0 TRN

X X X BSS

X X SPA

X X X SXP

OTHER 0 LAT N61

LONG+ RTGO EMS

+ VIO

I GET O.OSG

..

83

TABLE XI.- MANEUVER PADS - Concluded

(m) Lunar entry

LUNAR ENTRY

M I D P A c AREAI-- -

X X X X X X 0 0 0 R .OSG

X X X X X X 1 5 3 P .OSGX X X

.~X X X 0 0 1 Y .OSG

~I--

1 9 1 3 3 3 2 GET HOR

X N ACK

X X X X X P EI-17--,- I -0 - 0 1 5 1 1 LAT N61- --- +-t--f-I - 1 6 5 0 0 LONG-J

X X Xl --f- X X X 0 6 8 MAX G+*+~

3 1 0 V400K N60i-!

f-- -- 0 0 - 0 10 6 5 2 Y 400K+ + 1 2 2 2 0 RTGO EMS

+ + 3 6 I 3 9 0 VIOI-- -- '---- -- -1 ---r--

! , n 1· 5 i 0+ 3: 2 RRT-++ I .L 7xix Oi#2:8X X I • RET .05G' .~-

+ o '~~--L+ +100 NiA DL MAX

1-- N69+ 01 0: • I +~NIA DL MINI--t--rJ------T-

>-:;:-~ ! lirA VL MAX+I-- -- 1-""""1--1-- ~ VL MIN+ + I NI A--J--t-jX~xm

---X X X I DO

-- f-3_+.2

84

REFERENCES

1. Apollo Mission F (AS-505/CSM-I06/LM-4) Spacecraft OperationalTrajectory, Revision 1. April 28, 1969.

2. CSM/LM Spacecraft Operational Data Book, Volume III - Mass Properties.Amendment 34, November 1968.

3. CSM/LM Spacecraft Operational Data Book, Volume III - Mass Properties.Amendment 50, November 1968.

•

nasa · 2015. 3. 9. · msc internal note no. 69-fm-137 project apollo apollo mission f...

Documents