01 1,1 4. 'T i f, i

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

FINAL

FLIGHT PLAN APOLLO 8 AS-503/GSM- /03

NOV 79,1968

PREPARED BY FLIGHT PLANNING BRANCH FLIGHT CREW SUPPORT DIVISION

MANNED SPACECRAFT CENTER HOUSTON, TEXAS

APOLLO AS503/CSM 103 FINAL FLIGHT PLAN November 22, 1968

Submitted by:

Cr a

T. A. Guillory Flight Planning Branch

et,

Approved by: ,,,

W. J. North Chief, Flight Crew Support Division

,

Dona d'IC. Slayton Director of Flight Cre4 Operations

Concurrence:

Concurrence:

46/1.1-7// 2 George M. Low Manager, Apollo Spacecraft Program

/

Christophe JC. Kr qf t, Jr. Director of Fligh Operations Any comments or questions regarding this document should be forwarded to T. A. Guillory, Flight Planning Branch, Extension 4271, Mail Code CP34.

TABLE OF CONTENTS Page Introduction

ii

Abbreviations

iii Section I - General

1. Flight Plan Description

1-1

2. Flight Plan Notes

1-4

3. Scheduled Communication Tests

1-6

4. Update Forms

1-7 Section II - Detailed Timeline

1. Launch

2-i

2. Translunar Insertion

2-3

3. Lunar Orbit Insertion

2-51

4. Lunar Orbit Circularization

2-55

5. Transearth Insertion

2-71

6. Reentry

2-117 Section III - Consumables Analysis

1. SN-RCS

3-1

2. CM-RCS

3-40

3. SPS

3-41

4. Cryogenics

3 -42

5. Average Electrical Power Loads Section IV - Detailed Test Objectives

3-45

1. Test Objective Activities

4-1

2. Test Objective/Mission Activity Cross Reference

4-2

3. Test Objectives

4-8

Section V - Summary Flight Plan

5-1

INTRODUCTION

This Flight Plan has been prepared by the Flight Planning Branch, Flight Crew Support Division, with technical support by TRW Systems. This document schedules the AS503/CSM1O3 operations and crew activities to fulfill, when possible, the test objectives defined in the Mission Requirements, SA503JCSM103, C Type Mission, (Lunar Orbit). The trajectory Parameters used in this Flight Plan are for a December 21,1968 launch, with a 72° launch azimuth and were supplied by Mission Planning and Analysis Division as defined by the Apollo Mission C' Spacecraft Operational Trajectory. The Apollo 3 Flight Plan is under the configuration control of the Crew Procedures Control Board (CPCB). All proposed changes to this document that fall in the following categories should be submitted to the CPCB via a Crew Procedures Change Request: 1. Items that impose additional crew training or impact crew procedures. 2. Items that impact the accomplishment of detailed test objectives. 3. Items that result in a Significant RCS or EPS budget change. 4. Items that result in moving major activities to a different activity day in the Flight Plan. Items that require a change to the flight data file. The Chief, Flight Plnning Branch (FCSD) will determine what proposed changes fall in the above categories. Mr. T. A. Guillory will act as co-ordinator for all proposed changes to the Apollo 8 Flight Plan. This Flight Plan is not to be reproduced without the written approval of the Chief; Flight Crew Support Division.

ii

•

0

• •

0 ABBREVIATIONS

H.

Accelerometer ACCEL Activation ACT Acquisition ACQ Abort Electronics Assembly AEA Abort Guidance Sybsystem AGS Ampere Hours Ali ALIGN Alignment ALT Altitude AMP or amp Ampere AMPL Amplifier ANG Antigua Ant Antenna AOS Acquisition of Signal AOT Alignment Optical Telescope Ascent Propulsion Subsystem APS Atmosphere Revitalization ARS Ascension ASC Ascent AS CT Attitude ATT AUX Auxiliary AZ Azimuth BAT BDA BP BT Bio B iW BU BRKT

Battery Bermuda Barber Pole Burn time Bio-Medical Data on Voice Downlink Black & white Backup Bracket

CAL CAL CAM CB

Pt. Arquillo, California Calibration Angle Camera Circuit Breaker

ODE CDR CDU CIRC CK CM CMC CONT CMD CMP CNTL CNTLS C.O. C/O COAS COMM COMP CONFIG CP CR0 CRY 0 CSI CSM C&WS GYI

Constant Delta Altitude Commander Control Data Unit Circularization Check Command Module . Command Module Computer Continue Command Command Module Pilot Control Controls Cut off Check out Crew Optical Alignment Sight Communications Computational Configuration Control Point Carnarvon, Australia Cryogenic Coelliptic Sequence Initiation Maneuver Command Service Module Caution and Warning System Grand Canary Island

DAP D/B DEDA DEGS DEPL DET DIFF DK DOI

Digital Auto Pilot Deadband Data Entry and Display Assembly Degrees Depletion Determination or Digital Event Timer Difference Docked Descent Orbit Insertion

ABBREVIATIONS (Cont'd) DP S DSE DSKY DIO DUA DWN

Descent Propulsion Subsystem Data Storage Equipment Display and Key Board Detailed Test Objective Digital Uplink Assembly Down

E

ECS EPH EI ELDMK EMS ENU EPO EPS EQUIP EST EVAP EVT EXT

Erasable Environmental Control Subsystem Earth Far Horizon Earth (atmosphere) Interface Earth Landmark Entry Monitor System Earth Near Horizon Earth Parking Orbit Electrical Power Subsystem Equipment Eastern Standard Time Evaporator Extravehicular Transfer External

FC FDAI FLT FM FOV fps FQ FT or ft FTP

F Stop Fuel Cell Flight Director Attitude Indicator Flight Frequency Modulated Field of View Feet per second Flight Qualification Feet Full Throttle Position

GBI GDC GDS

Grand Bahama Gyro Display Coupler Goldstone, California

GET GETI GLY GMT G&N GNCS GWM GYM

Ground Elapsed Time Ground Elapsed Time of Ignition Glycol Greenwich Mean Time Guidance and Navigation Guidance Navigation Control System Guam Guaymas, Mexico

HA HAW HBR HD HGA HI Hp HSK HTR HTV

Apogee Altitude Hawaii High Bit Rate (TLM) Highly Desirable High Gain Antenna High Perigee Altitude Honeysuckle (Canberra, Australia) Heater USNS Huntsville

ID IGN IAN INIT INT IP IU I VT

Identification Ignition Inertial Measurement Unit Initialization Intervalometer Initial Point Instrumentation Unit Intravehicular Transfer

JETT

Jettison

kwh

Kilowatt Hour

Latitude LAT LBR Low Bit Rate (TLM) LBS or lbs Pounds

0 •

0 ABBREVIATIONS (Cont'd)

LCG LDG LDMK LEB LFH LGC LH L/H LHEB LHFEB LION LLM LLOS LM LMP LNH LOT LONG LOS LPO LR LT LTG LV L/V LVPD .

Liquid Cooled Garment Landing Landmark Lower Equipment Bay Lunar Far Horizon LM Guidance Computer. Left-hand Local Horizontal Left-hand Equipment Bay Left-hand Forward Equipment Bay Lithium Hydroxide Lunar Landing Mission Landmark Line of Sight Lunar Module Lunar Module Pilot Lunar Near Horizon Lunar Orbit Insertion Longitude Loss of Signal Lunar Parking Orbit Landing Radar Light Lighting Launch Vehicle Local Vertical Launch Vehicle Pressure Display

M

Mandatory Madrid, Spain Manual Maximum Maximum Dynamic Pressure Midcourse Correction Mission Control Center,- Houston Main Display Console

MAD MAN MAX MAX Q MCC MCC-N MDC

MEAS MER MET M/I MIN MLA MNVR MON MSFN MTVC

Measurement DSNS Mercury Mission Event Timer Minimum Impulse Minimum Merritt Island Maneuver Monitor Manned Space Flight Network Manual Thrust Vector Control

NAV NCC NOM NSR NXX

Navigation Corrective Combination Maneuver Nautical Miles Nominal Nominal Slow Rate Noun XX

OBS 0/F OP ER ORB ORDEAL ORIENT OVHD

Observation Oxidizer to Fuel Operate Orbital Orbit Rate Display Earth and Lunar Orientation Overhead

P PAD PCM PC PGA PCNCS PIPA PM P OL

Pitch Voice Update Pulse Code Modulation Pericyntiian Pressure Garment Assembly Primary Guidance Navigation Control Section Pulse Integrating Pendulous Accelerometer Phase Modulated Polarity or Polarizing

TIM

ABBREVIATIONS (Cont'd)

PREF PREP PRESS PRIM PT PRN PROP PU PUGS PTC PWR Pxx

Preferred Preparation Pressure Primary Point Pseudo-Random Noise Proportional Propellant Utilization Propellant Utilization and Gaging System Passive Thermal Control Power Program XX

Qty

Quantity

R R&B RAD RCDR RCS RCU RCV RED REFSMMAT REG REQD RH RNDZ RR RSI RT RTC Rxx

Roll Red & Blue Radiator Recorder Reaction Control Subsystem Remote Control Unit Receiver USNS Redstone Reference Stable Member Matrix Regulator Required Right-hand Rendezvous Rendezvous Radar Roll Stability Indicator Real Time Real-Time Command Routine XX

0

S SA S/C SCE SCS SCT SEC SECO SEP SEQ SLA SLOS SM SPOT SPS SR SRX SS STX STBY Sw SXT SYNC

Shaft Shaft Angle Spacecraft Signal Conditioning Equipment Stabilization Control System Scanning Telescope Secondary S-IVB Engine Cut-off Separate Sequence Service Module LM Adapter Star Line-of-Sight Service Module Spot Meter Service Propulsion System Sunrise S-Band Receiver Mode No. X Sunset S--Band Transmit Mode No. X Standby Switch Sextant Synchronization

T T

Trunnion Time of Ephemeris Update

EPHEM TA TAN TCA TBD TEC TEI

Trunnion Angle Tananarive Time of Closest Approach To Be Determined Trans Earth Coast Transearth Insertion

0

ABBREVIATIONS (Cont' d)

TEMP TERM TEX T &D TGT TIC TLC TLI TLM TPF TPI TPM T/R TRANS TV TVC TWR

Temperature Terminate Corpus Christi, Texas Transposition and Docking Target Time of Ignition Trans Lunar Coast Translunar Insertion Telemetry TeLwinal Phase Final Terminal Phase Initiation Terminal Phase Midcourse Transmitter/Receiver Translation Television Thrust Vector Control Tower

UMB UNDK US

Umbilical Undock United States Pass

VHF VLV Vxx

Very High Frequency Valve Verb xx

W/0 WRT WTN

Without With Respect to USNS Watertown

XFER XMIT XPONDER

Transfer Transmit or Transmitter Transponder Yaw

AV AV C AR

Velocity Change (Differential) Velocity Change at Engine Cutoff Position Change (Differential)

8-balls LBS or lbs

Flight Director Attitude Indicator (FDAI) Pounds

CAMERA NOMENCLATURE

2/80/B3 - Hasselblad No. 2/80mm Lens/Stowage Location 16/18/20 - 16mm Camera/18mm Lens/20 Frames Per Second 1/150/New B&W/INT - Hasselblad No. 1/150mm Lens/VSE New B&W Magazine/with interferometer C-EX - color film - external Polarization filter, Shutter Speed 1/4 POL FILTER 1/4 S0368 - Type of External Film 2/80/H.S. - Hasselblad No. 2/80mm Lens/High Speed Film Cable/BRRT/R&B - Use Power Cable, Camera Mounted on Bracket with Red & Blue Filter -

LUNAR TERMINATOR

S

N

SPACECRAFT SUNSET

ESFN LOS DARKNESS SPACECRAFT SUNRISE LUNAR TERMINATOR WINDOW (HEADS UP)

S-DAND EGA OPTICS LUNAR SURFACE POINT MSPN AOS EARTH

viii

SECTION I - GENERAL

e e

e

•

•

FLIGHT PLAN DESCRIPTION DAY 1

The spacecraft is launched into a 100-nm circular orbit with a launch azimuth that varies between 72° and 108° during the daily launch window. The lift-off time varies during the monthly launch window, but is constrained to daylight launches. The trajectory for this flight plan is a 72° launch azimuth December 21, 1968 with a 12:51:00 GMT (7:51:00 AM, EST) lift-off. Both the variable lift-off time and launch azimuth effect the earth-orbit station coverage, INN alignment time, translunar and transearth coast time, and lunar surface lighting conditions. The spacecraft remains attached to the S-IYB for approximately 4 hours. During this time, the crew checks out the OSM systems, performs an optics check, IMU realignment to the pad REFSMMAT, monitors the TLI maneuver, and performs transposition and separation from the S-IVB. The crewmen doff and stow their helmets and gloves prior to TLI and they are not donned again. The TLI maneuver places the S/C in a free return lunar trajectory. Following TLI, the CAP doffs his PGA, performs an IMU realign,'and a series of star/earth horizon sightings. All translunar and transearth sightings contain three marks per set. After these sightings, the CDR and LMP doff and stow their PGA's. At this point, the first eat period is scheduled.

•

At TLI + 6 hours (09:00 GET), the first MCC decision point is scheduled. Before this point and prior to each midcourse, there is a MCC-H state vector update, target load, maneuver pad update, an IMU alignment, and systems checks. For the nominal trajectory, the midcourses are nominally zero. a series of star/earth landmark sightings is scheduled at which MCCl' time the CDR sleep period begins (11:00 GET) followed by the CMP and LMP sleep period (18:00 GET). During the CDR sleep period, the CAP performs a series of star/earth horizon sightings. After

DAY 2

•

Crew activity on day .2 begins at approximately 24:00 GET. At 26:30 GET, the CMP performs a series of star/earth horizon sightings, then MCC 2 at TLI + 25 hours (28:00 GET), followed by another series of star/earth horizon sightings. Then the CDR sleep period begins (29;00 GET) followed by the CMP and LMP sleep period (36:00 GET). During the CDR sleep period, TV is scheduled for 15 minutes (31:15 GET) and a series of star/earth horizon sightings is performed at (34:15 GET). During day 2, MCC 3 occurs at LOI -22 hours (47:00 GET). The maneuver is preceded by a series of star/earth horizon sightings.

1-1

DAY 3

Crew activity on day 3 begins at approximately 48:00 GET. During the CDR sleep period (52:00 GET), the CMP performs a series of star/lunar horizon sightings (52:15 GET) and TV is scheduled for 15 minutes (55:15 GET). At LOT - 8 hours (61:00 GET), MCC is scheduled. The OMP and LMP sleep period 4 (62:00 GET) is scheduled between MCC 4 and LOI 1 . At 69:07 GET, the LCI

maneuver places the S/C into a 60 x 170-nm lunar I orbit. Scheduled during the first two lunar revolutions are camera preparation, eat period, COAS ground track determination, control point and pseudo landing site, observations, photographs of targets of opportunity, TV transmission, and L01 2 preparation. The IMU is realigned once during each dark period in lunar orbit. DAY 4

Crew activity on day 4 begins at approximately 72:00 GET. At 73:31 GET, the LOI 2 circularization maneuver places the S/0 into a 60-am circular orbit. Scheduled during revolutions 3 and 4 are a 2-hour CMP rest period, landmark training photography, vertical stereo photography, and landmark lighting evaluation. Scheduled during revolutions 5 and 6 are a 3-hour CDR rest period, one control point landmark tracking, and a pseudo landing site tracking during each daylight period. Each tracking consists of 4 marks. Scheduled during revolutions 7 and 8 are a 2-hour LMP rest period, three control point landmark trackings, and a pseudo landing site tracking during each daylight period. Each tracking consists of 4 marks. Scheduled during revolutions 9 and 10 are a 2-hour OMP rest period, convergent stereo photography, an eat period, TEl preparation, and the TEl maneuver at 89:15 GET.

After TEI, the CDR sleep period begins (89:20 GET) followed by the CMP and the DMP sleep period (94:00 GET). During the CDR sleep period, the CMP performs a. series of star/lunar horizon sightings. DAY 5

Crew activity on day 5 begins at approximately 96:00 GET. After the sleep period, the CMP performs a series of star/lunar horizon and star/earth horizon sightings; then MCC at TEI 15 hours (104:00 GET), followed by 5 TV transmission at 104:15 GET and a series of star/earth horizon sightings (105:15 GET). During the CDR sleep period (105:00 GET), the CMP performs a series of star/lunar horizon and star/earth horizon sightings. The CMP and LMP sleep periods begin at 112:00 GET. 1-2

410

•

DAY 6 Crew activity on day 6 begins at approximately 120:00 GET. After a series of star/earth horizon sightings, MCC 6 is scheduled at TEI 33 hours (122:00 GET) followed by a series of star/lunar horizon and star/earth horizon sightings. Also scheduled is the CDR sleep period (127:00) and both the CMP and IMP sleep periods (134:00). During the CDR sleep period, TV transmission is scheduled (128:00 GET), and the CMP performs a series of star/earth horizon and star/lunar horizon sightings. After the sleep period, the CMP does a series of star/earth horizon sightings. DAY 7 Crew activity on day 7 begins at approximately 144:00 GEI'. At El minus 2 hours (144:50 GET), MCC 7 is scheduled. CM/SM separation nominally occurs at 146:35 GET with splashdown in the Pacific Ocean approximately 20 minutes later.

FLIGHT PLAN NOTES A. CREW 1. Crew designation is as follows:

Designation

Couch Postion

Commander (CDR) Command Module Pilot (CMS) Lunar Module Pilot (LMP)

Left Center Right

Prime

Backup

Borman Armstrong Lovell Aldrin Anders Haise

2. The crew will nominally follow a 17-hour work/7-hour rest cycle where possible. One crewman will be awake at all times with all crewmen awake during major burns. The crew will eat together when possible with additional activities held to a minimum during eat periods. The eat period is normally one-hour duration. -

3. The pressure suits will be doffed after TLI and donned prior to entry. Helmets and gloves will be doffed prior to TLI and will remain off until prior to entry. 4. A crew status report will be made twice a day on each crewman. 5. General flight plan updates containing changes to the following day's activity schedule, will be voiced up once per day. 6. Negative reporting will be used in reporting completion of each checklist. B. COMMUNICATIONS AND INSTRUMENTATION

1.

S-band will be prime for voice, ranging and PCM with the VHF used as backup for voice during near earth phases (< 4000 nm). The S--band backup voice system will be checked during the first orbit and the high gain antenna checked after S-I'VB/CSM separation.

2. The Flight Qual Recorder will be used as follows: a. b. c. d.

Lift-off -45 seconds through 0:12:00 GET TLI -2 minutes through TLI cutoff +1 minute CSM/S-IVB Sep -2 minutes through Sep +1 minute LOI -2 minutes to end of tape 1

3. The DSE will normally be dumped by real time command (RTC). 4. During communications, the spacecraft will be referred to as 'Apollo 8" and the ground as "Houston". The crew member call sign will be their assigned crew position. O. CSM SYSTEMS 1. The spacecraft . (S/C) lift-off switch positions are listed in Apollo (CSM 103) Operations Handbook (AOH), Volume 2, August 1, 1968. 2. Fuel cell purging for H2 and 0 2 will be scheduled R/T. 3. The S/C will remain fully poweredup throughout the mission (IMU, 0M0 and SOS always in operate) with the optics on as required. 4. IMU drift checks are scheduled. after TLI, before LOIl' on revolutions 2 and 4 through 10 in lunar orbit, and prior to entry. 5. The potable water is chlorinated at 24-hour intervals. 6. All onboard gage readings will be mead directly from the spacecraft gages and not corrected by the appropriate factors.

SCHEDULED COMMUNICATION TESTS GET

ALTITUDE nm

03:20

CSM ANTENNA

SIGNAL COMBINATION

GROUND ANT

COMMUNICATIONS MODE

OMNI

4.2

85' GDS

Carrier,PRN,voice, 51.2 KBPS TM

05:45

24,000 24,000 24,000

HI GAIN HI GAIN HI GAIN

4. 2 6.2 .2

85' GDS 85' GDS 85' GDS

Carrier,PRN,voice, HBR TM Oarrier,PRN,Voice, HBR TM Plybk of Recorded Voice & LBR TM

07:00 to 08:00

35,000 35,000 35,000 35,000

HI HI HI HI

4.3

85' 85' 85' 85'

Carrier,PRN,voice, LBR TM Carrier,PRN,voice, LBR TM Carrier,PRN,voice HBR TM Carrier,voice and LBR TM

29:00 to 30,000 or 125,000 to 126,000

GAIN GAIN GAIN GAIN

110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000 110,000

HI GAIN HI GAIN HI GAIN HI GAIN HI GAIN HI GAIN HI GAIN HI GAIN OMNI OMNI OMNI OMNI OMNI OMNI

31:15

120,000

HI GAIN

69:00

205,000 205,000 205,000

HI GAIN HI GAIN HI GAIN

89:00

205,000

HI GAIN

6.3 5.2 8.1

GDS GDS GDS GDS

30' ASC 30' ASC

4 5 6 8

4.2 5.2 4.3 8.1 1

.5 .6

1.7 .8 .10

30' 30' 30' 30' 30' 30' 30' 30' 30' 30' 30' 30'

ASC ASC ASO ASC ASC ASC ASO ASC ASC ASC ASC ASC

Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier, Carrier,

PRN, Voice PRN, Updata PRN, Voice, Updata BU Voice PRN, Voice, HER TM PRN, Voice, HBR TM PRN, Voice, LBR TM Voice, HBR TM PRN LBR TM Key Subcarrier PRN Ranging BU Voice, LBR TM BU Voice

85' GDS CSM Television .4 NORMAL OPERATING MODES 6.2 Carrier, PRN, Voice, HBR TM 85' 6.3 85' Carrier, PRN, Voice, LBR TM .2 Plybk of Recorded voice &LBR TM 85' 85'

.4

1-6

CSM television

Pages 1-8 thru 1-21 contain the following voice update forms and the explanation for the abbreviations and symbols used. Pg 1-8 and 1-9

TLI PAD/EXPLANATION

Pg 1-10 and 1-11

P27 UPDATE PAD/EXPLANATION

Pg 1-12 thru 1-14

MANEUVER PAD/EXPLANATION

Pg 1-15 thru 1-17

ENTRY PAD/EXPLANATION

Pg 1-18 thru 1-21

MAP UPDATE PAD/EXPLANATION

TLI X

• •

;

; X . X

X

x

x

x

X

X

X

X

X

X

X

X

X

;

•a

X

TB6p IR

X X X

H i

X

XX

.

Y

X X X

;

BT ,

• +

'

+

P

.8VC I VI

X X

X

X , X ,. X

X

X

X

X XX

X

X

X

XX

X

. -

R SEP P SEP Y SEP

TLI PAD TB6p

X:XX:XX(HRS:MIN:SEC)

PREDICTED TIME OF BEGINNING OF S-IVB RESTART PREPARATION FOR TLI IGN -9 MIN) TLI (TB6

R Y

XXX (DEG) XXX (DEG) XXX (DEG)

PREDICTED SPACECRAFT IMU GIMBAL ANGLES AT TLI IGNITION

BT

XX:XX (MIN:SEC)

DURATION OF TLI BURN

AVC'

XXXXX.X (fps)

NOMINAL TLI AV SET INTO EMS AV CONTROL

VI

+XXXXX (fps)

NOMINAL INERTIAL VELOCITY DISPLAYED ON DSKY AT TLI CUTOFF

R SEP P SEP Y SEP

XXX (DEG) XXX (DEG) XXX (DEG)

PREDICTED SPACECRAFT IMU GIMBAL ANGLES AT COMPLETION OF S-IVB MNVR TO CSM/S-IVB SEP ATTITUDE

P27 UPDATE PURP

V

GET 304 0

V

•

•

INDEX

INDEX

•

IS INDEX

02 03 04 05 06 F

1--

07 10 II 12 13 14 15

'

16 17 20 2I 22 23 24 N34

HRS

X X

MIN

X X XX

X

X X

X•X

NAV CHECK SEC N43

LAT

0

X

X X X X•X

X •

0,

•

LONG ALT

+ 0

1-b

I

, +

0

'

_•

1

•

P27 UPDATE PURP

XXX

TYPE OF DATA TO BE RECEIVED (SUCH AS: NAV - LIFT-OFF TIME)

V

XX

TYPE OF COMMAND LOAD (70 - 71 - 72 - 73)

GET

XXX:XX:XX(HR:MIN:SEC)

TIME DATA RECORDED

01

XX (OCTAL)

INDEX NO. OF COMMAND WORDS IN LOAD

02-24 XXXXX

NO. OF CORRECTION COMMAND WORDS

NAV CHECK

TO CONFIRM POINT ABOVE GROUND TRACK FOR A GIVEN TIME

T

XX:XX:XX(HRS:MIN:SEC)

TIME

LAT

XX:XX (DEG)

LATITUDE

LONG

XXX:XX (DEG)

LONGITUDE

ALT

XXX.X (nm)

ALTITUDE

MANEUVER •

PUR;'051::

NDRTH L SOUTH SET STARS

P.S'OP/GUk:)

R ALIGN P ALIGN Y ALIGN

WT

;. J 47

"8

0

0

PTRhA

0

0

YTRI: A

I+

0

0

HRS GET

+

0

0

WN N33

+

0

SEC

ULAGE

nvx

U

X X

X

X

X

X

HX X

X

•

LIVy

•

nVZ

NE-1

R

N4-3- 1

P • :]VT

•

HORIZON/WINDOW

XXX

•

i3T .]VC

X X

SXTS

XX X •

0 SFT . 0 SRN BSS

X X X

X

X

• ,

XX OT H ER

SPA SXP

XI

LAT

0

N61

LONG 11/_----,L--

RTGO

EMS

VIO •

•

1-12

•

•

I GET

.05G

MANEUVER PAD PURPOSE

XXXXXX

PROP/GUID

TYPE OF MNVR TO BE PERFORMED PROPULSION SYSTEM (SPS/RCS)/ GUIDANCE (SCS/G&N)

WT

XXXXX (lbs)

PREMANEUVER VEHICLE WEIGHT

P TRIM

X.XX (DEG)

SPS PITCH GIMBAL OFFSET TO PLACE THRUST

Y TRIM

X.XX (DEG)

SPS YAW GIMBAL OFFSET TO PLACE THRUST

GETI -

XX:XX:XX (HRS:MIN:SEC)

TIME OF MNVR IGNITION

AVX AVY AVZ

XXXX.X (fps) XXXX.X (fps) XXXX.X (fps)

P30 VELOCITY TO BE GAINED COMPONENTS IN LOCAL VERTICAL COORDINATES

R

XXX (DEG) XXX (DEG) XXX (DEG)

IMU GIMBAL ANGLES OF MANEUVER ATTITUDE

HA

XXXX.X (nm)

PREDICTED APOGEE ALTITUDE AFTER MANEUVER

HP

XXXX.X (nm)

PREDICTED PERIGEE ALTITUDE AFTER MANEUVER

XXXX.X

TOTAL VELOCITY OF MANEUVER

BT

X:XX (MIN:SEC)

MANEUVER DURATION

AVC

XXXX.X (fps)

PREMANEUVER AV SETTING IN EMS AV COUNTER

SXTS

XX (OCTAL)

SEXTANT STAR FOR MANEUVER ATTITUDE CK

SFT

XXX.X (DEG)

SEXTANT SHAFT SETTING FOR MANEUVER ATTITUDE CK

TRN

XX.X (DEG)

SEXTANT TRUNNION SETTING FOR MANEUVER ATTITUDE CK

BSS

XXX (OCTAL)

BORESIGHT STAR FOR MANEUVER ATTITUDE CK USING THE COAS

SPA

XX.X (DEG)

BSS PITCH ANGLE ON COAS

P Y

AVT

1-13

MANEUVER PAD

(cont'd)

SXP

X.X (DEG)

BSS X POSITION ON COAS

LAT LONG

XX.XX XXX.XX

LATITUDE AND LONGITUDE OF THE LANDING POINT FOR ENTRY GUIDANCE

RTGO

XXXX.X

RANGE TO GO FOR EMS INITIALIZATION

VIO

XXXXXX (fps)

INERTIAL VELOCITY AT .05G FOR EMS INITIALIZATION

GET(.05G)

XX:XX:XX

TIME OF .05G

NORTH & SOUTH SET STARS

STARS FOR TELESCOPE FOR BACKUP GDC ALIGN

R, P, Y ALIGN)

ATTITUDE TO BE SET IN ATTITUDE SET TW FOR BACKUP GDC ALIGN

ULLAGE

NO. OF SM RCS JETS USED AND LENGTH OF TIME OF ULLAGE

HORIZON WINDOW

WINDOW MARKING AT WHICH HORIZON IS PLACED AT A SPECIFIED TIG (ATT CK)

(

ENTRY AREA

xIxIx x xxix

•

R .05G

X

X

X

X

X

P .05G

X

X

X

Y

.05G

GET X

XX

P

0

LAT

HOR CK N6 I

LONG MAX G

X X

V400K N60

,

0 0

0

0

T4OOK

+

RTGO

+

•

VIO

4- 1

••

•

•

•

xx 0

+

0

+

0 0

X

X

+

0

'

+i 0

.

EMS

RRT

••

RET. 05G *

••

DL MAX *N69 DL M IN

0 0

VL MAX * *IVLMN

XX X

X.X

X

• • •

X

XX

X

• •

X

X

4 X. X , X

x x: •

•

XX

Do

X

X :X . X X

X

X •

X

X

RET VCIRC

••

RETB BO

• •

RETEBO RETDRO SX TS

X X

SFT !O XX

;0

0 X

X

X

TRN

X

BSS • _ SPA SXP •

X

XX

XXX

XX

X

X X X X.

X

X

X

1-15

0

X

LIFT VECTOR

ENTRY PAD AREA

XXX

SPLASHDOWN AREA DEFINED BY TARGET LINE

R .05G P .05G Y .050

XXX(DEG) XXX(DEG) XXX(DEG)

SPACECRAFT IMU GIMBAL ANGLES REQUIRED FOR AERODYNAMIC TRIM AT .050

GET (H0R CK)

TIME OF ENTRY ATTITUDE XX:XX:XX (HRS:MIN:SEC). HORIZ CHECK AT EI -17 MIN.

P (HOR CK)

XXX(DEG)

PITCH ATTITUDE FOR HORIZON CHECK AT EI -17 MIN

LAT

±XX.XX(DEG)

LATITUDE OF TARGET POINT

LONG

±XXX.XX(DEG) LONGITUDE OF TARGET POINT

MAX G

XX.X (G's)

PREDICTED MAXIMUM REENTRY ACCELERATION

V 400K

XXXXX (fps)

INERTIAL VELOCITY AT ENTRY INTERFACE

Y400K

X.XX(DEG)

INERTIAL FLIGHT PATH ANGLE AT ENTRY INTERFACE

RTGO

+XXXX.X(nn)

RANGE TO GO FROM .05G TO TARGET FOR EMS INITIALIZATION

VIO

+XXXXX.(fps)

INERTIAL VELOCITY AT .05G FOR EMS INITIALIZATION

RRT

XX:XX:XX (HRS:MIN:SEC)

REENTRY REFERENCE TIME BASED ON GET OF PREDICTED 400K (DET START)

RET .05G

XX:XX (MIN:SEC)

TIME OF .05G FROM 400K (RRT)

D L MAX

X.XX (G's)

D MIN

X.XX (G's)

MAXIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC) MINIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC)

V MAX

XXXXX (fps)

MAXIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC)

V MIN

XXXXX (fps)

MINIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC) 1-16

ENTRY PAD (cont'd) DO

X.XX (G's)

PLANNED DRAG LEVEL DURING CONSTANT G

RET V CIRC

XX:XX (MIN:SEC)

TIME FROM EI THAT S/C VELOCITY BECOMES CIRCULAR

RETBBO

XX:XX (MIN:SEC)

TIME FROM EI TO THE BEGINNING OF BLACKOUT

RETEBO

XX:XX (MIN:SEC)

TIME FROM EI TO THE END OF BLACKOUT

RETDRO

XX:XX (MIN:SEC)

TIME FROM ET TO DROGUE DEPLOY

SXTS

XX(OCTAL)

SEXTANT STAR FOR ENTRY ATTITUDE CHECK

SFT

XXX.X(DEG)

SEXTANT SHAFT SETTING FOR ENTRY ATTITUDE CHECK

TRN

XX.X(DEG)

SEXTANT TRUNNION SETTING FOR ENTRY ATTITUDE CHECK

BSS

XXX(OCTAL)

BORESIGHT STAR FOR ENTRY ATTITUDE CHECK USING THE COAS

SPA

XX.X(DEG)

BSS PITCH ANGLE ON COAS

SXP

X.X(DEG)

BSS X POSITION ON COAS

LIFT VECTOR

XX

LIFT VECTOR DESIRED AT .05G's BASED ON ENTRY CORRIDOR

MAP UPDATE REV 1/2 GET (hrs:min:sec) LOS

REMARKS

PM AOS SS LOS SR PM AOS SS

REV 2/3

REMARKS

GET (hrs:min:sec) LOS SR PM AOS SS

REV 3/4 .

REMARKS

GET (hrs:min:sec) LOS SR PM AOS SS

1-18

MAP UPDATE

•

REV 7/8 GET (hrs:min:sec) LOS PM AOS SS

•. -.

.• -. ..

REV 8/9 GET (hrs:min:sec) LOS . .• SR PM ' AOS .SS

REV 9/10 GET (hrs:min:sec) LOS •— -. SR PM AOS SS

REMARKS

REMARKS

.• : : -.

REMARKS

' . '

REV 10 GET (hrs:min:sec) LOS .• SR • ADS •. SS '

REMARKS

1-19

MAP UPDATE REMARKS

REV 4/5 GET (hrs:min:sec) LOS .• ' .• SR •' . PM AOS SS

•

•

REV 5/6

REMARKS

GET (hrs:min:sec) LOS . SR . PM

.•

AOS

:

. .-

SS

REV 6/7 GET (hrs:min:sec) . LOS

REMARKS *

SR

•.

PM

.

•

•.

AOS

.•

.•

SS

.•

1-20

MAP UPDATE

•

LOS

XX:XX:XX(HRS:MIN:SEC)

TIME OF MSFN LOSS OF SIGNAL IN LUNAR ORBIT

AOS

XX:XX:XX(HRS:MIN:SEC)

TIME OF MSFN SIGNAL

SS

XX:XX:XX(HRS:MIN:SEC)

TIME

SR

XX:XX:XX(HRS:MIN:SEC)

TIME OF SPACECRAFT SUNRISE IN LUNAR ORBIT

PM

XX:XX:XX(HRS:MIN:SEC)

TIME OF CROSSING OF MOON'S PRIME MERIDIAN (150°W)

ACQUISITION OF

OF SPACECRAFT SUNSET IN LUNAR ORBIT

• 1-21

•_:..

•

SECTION II - DETAIL-RD TTNELIn

e

•

e

•

•

0 0

0 FLIGHT PLAN

,

-00:45

LMP:

FLT RCDR - RECORD

-00:09

LCC:

IGNITION COMMAND L/V ENGINE LTS (5) - OUT

-00:01 00:00

REMARKS

EVENT

TIME

LCC:CDR:

LIFT-OFF LT - ON, MET STARTS COUNT

REPORT LIFT-OFF P11 AUTO

00:02

CDR:

REPORT YAW MNVR

00:11

CDR:

REPORT ROLL AND PITCH PROGRAM

,

INITIATE CDR

REPORT ROLL COMPLETE

MCC-H:CDR:

REPORT MARK MODE 1B

00:50

LMP:

REPORT CABIN PRESS DECREASE

01:17

CDR:

REPORT MAX Q

01:50

MCC-H:CDR:

REPORT MARK MODE 10

02:00

MCC-H:CDR:

REPORT GO./NO GO FOR STAGING

02:05

CDR:

REPORT INBOARD ENGINE CUTOFF

02:31

CDR:

REPORT OUTBOARD ENGINE CUTOFF

LTS 1, 2, 3, & 4 - ON

02:32

CDR:

REPORT S-IC/S-II STAGING

LTS OFF

00:28 .00:42

MISSON AS503/103 MSC FORM 2114C (JUL 67)

EDITION

FINAL

DATE November 22,1968

PAGE 2-1

FLIGHT PLAN REMARKS

EVENT

TIME

03:00

CDR:

REPORT 2ND PLANE SEP

03:07

CDR:

REPORT TWR JETT & MODE II

03:25

CDR:

REPORT GUIDANCE INITIATE

03:53

MCC-H:

REPORT TRAJECTORY AND GUID.

>65% THRUST-S-II SEP LIGHT OUT

GO/NO GO 04:00

CMP:

REPORT S/C GO/NO GO

05:00

LMP:

REPORT S/C GO/NO GO

05:53

MCC-H:CDR:

REPORT S-IVB TO ORBIT CAPABILITY

06:00

CDR:

REPORT S/C GO/NO GO

06:15

LMP:

OMNI ANT-D

CDR:

REPORT S/C GO/NO GO

08:20

MCC-H:CDR:

REPORT GO/NO GO FOR STAGING

08:40

CDR:

REPORT S-II CUTOFF,

IF LAUNCH AZIMUTH •

3

BURN CHART

LOI 2

P or Y RATES

ATT DEVIATION

SHUTDOWN TIME

10°/SEC TAKEOVER

10° TAKEOVER

B/T +1 SEC

RESIDUALS NO TRIM

,V gx 1V gY V gz AV C FUEL j)); :UNBALANCE

REMARKS:

0

0 0

•

0

0 • FLIGHT PLAN

73:00 -MNVR TO BURN ATT GO INERTIAL

73:0•

b

2/80/B&W, 1/250 16/18/C EX, 1/250 F CHART, 6 fps, BRACK

SXT STAR CK TRANSFER TO COUCH

73:09

MCC—H

LIMP

CMP •

CDR

1/150/B&W, 1/60, CHART, BRKT PRE LOI SYSTEMS CKS

73:17

GOC ALIGN TO IMU

SM RCS MONITOR CK GETI = 73:30:54 AV = 138.5 fps BT = 9.7 SEC

BEGIN REV 3

SPS MONITOR CK

GDC ALIGN TO IMU/ORB RATE (60 nm)

V66 TRANS CSM STATE VECTOR TO LM SLOT SM RCS MONITOR CK

ROLL RIGHT 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC (HEADS OWN TRACKING ATT) ORDEAL 180, 308, 0 BEGIN ORB RATE

INITIATE BAT CHARGE

ACQUIRE S/C V64 ACQUIRE MSFN ON HGA

73:48 LOI 2BURN STATUS REPORT

PIPA BIAS CK

REST PERIOD (2 HOURS)

BIOMED Sw - RIGHT 74:00 MISSION

EDITION

AS503/103

FINAL

MSC Fun 1910 (Nov 69)

TIME

DATE

November 22, 1962

73:00 - 74:00

FLIGHT PLANNING BRANCH

1

DAY/REV

PAGE

4/LPO

2-55

FLIGHT PLAN LMP •

CMP

CDR •

MCC—H

TRAINING PHOTOGRAPHY

'TRAINING PHOTOGRAPHY

PITCH UP TO TRACK LDMK

START CAMERAS 7 MIN PRIO LDMK 70mm - 20 SEC INT UNTIL TRACKING - THEN 5 SEC F STOP FROM CHART

7

4 : 1

,70mm & 16mm

5:

74:17 STOP CAMERA

STOP CAMERAS

PITCH DWN TO HEADS DWN TO REACQUIRE MSFN ORDEAL 180, 0, 0 GO INERTIAL

1/80/HS, 1/4, F 2.8 VERIFY SYSTEMS STATUS REST PERIOD (2 HOURS)

RECORD MAP UPDATE

VOICE UPDATE: MAP UPDATE 3/4 DUMP DSE

IMU REALIGN P52 REFSMMAT OPTION 3 AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF TORQUE ANGLES: X

Y

I

INSTALL 16 MM CAMERA GDC ALIGN TO IMU RECORD BLOCK DATA (TEI 3 & TEI 4 )

•

75:00 =I MISSION

AS5L3/103 MSC Form 1810 (Nov 88)

EDITION

LINAI

a

r"-^",„,,o

DATE

November 22, 1968 FLIGHT PLANNI

TIME

74:00 - 75:00

VOICE UPDATE: BLOCK •DATA

DAY/REV

PAGE

4/LPO

2-56

FLIGHT PL AN 75:00

PITCH UP TO VERTICAL AT 0.2°/SEC (+Z FWD) ORDEAL 180, 270, O. BEGIN ORB RATE

1/80/NEW B&W, 1/250, F 2.8 BRKT/INT 2/150/B&W

16/18/NEW C EX/1 fps 1/250, F 2, 1 fps START CAMERA S/S SR 46 MIN

75:09 75:15

MCC—H U

LMP

CMP

CDR

•

START CAMERA 1 S/C SR 6 MIN

VERTICAL STEREO PHOTOGRAPHY EXTRA EXP EACH 5 MIN - NOTE TIME REST PERIOD (2 HOURS)

75:30 BEGIN REV 4 SUBSOLAR POINT 75:46 ROLL RIGHT 180° AT 2°/SEC (-Z. FWD) MAINTAIN ORB RATE

75:46

INSTALL SXT BRKT & 16mm CAMERA. TAKE PHOTOS AS TIME PERMITS,

ACQUIRE MSFN ON

ACQUIRE S/C

QMNI ANT SA 0° TA 0 ° 76:00 MISSION

AS503/103 MSC Form 1910 (Nov 68)

EDITION

FINAL

TIME

DATE

November 22, 1968

75:00 - 76:00

FLIGHT PLAMNING BRANCH

DAY/REV

4/LPO

PAGE

2-57

FLIGHT PLAN CALF T

CDR

76:0

PITCH UP AT 0.2°/SEC TO 0, 35, 5, 0

IPI ACQ

76:15

• .

.

..

.

.•

.

{LDMK LIGHTING EVALUATION (THRU OPTICS) OF LDMK 81

STOP CAMERAS AT TERMINATOR

MCC-H

AT PITCH UP 1/80/B&W, 1/250, F 11

.

IPII ACQ

BEGIN ORB RATE

LMP

STOP CAMERA 1 AT TERM RECORD MAP UPDATE

VOICE UPDATE: MAP UPDATE 4/5 P27 UPDATE: STATE VECTOR

V64 ACQUIRE MSFN ON HGA

ACQUIRE S/C

76:21

ROLL RIGHT 180° AT 2°/SEC (HEADS DWN) GO INERTIAL

76:30 —1

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF , — --

S F

EAT PERIOD GDC ALIGN TO IMU

1/80/HS, 1/4, F 2.8 '(20 SEC STRIP - 20 EXP) VERIFY SYSTEMS STATUS RECORD BLOCK DATA: (TEI 4 & TEI 5 )

TORQUE ANGLE S : X Y Z . 1

AS503/103 MSC Form 1910 (Nov 68)

•

0

EDITION

FINAL

VOICE UPDATE: BLOCK DATA

TRANS TO LEFT COUCH

1/80/B&W, 1/250, F 2.8 INT (CDR). BIOMED Sw - CENTER

76:58 77:00 MISSION

DUMP DSE

TIME

DATE

November 22, 1968

76:00 - 77:00

FLIGHT PLANNING BRANCH

DAY/ REV

4/LPO

PAGE

2-58

0 FLIGHT PLAN 77:00

•

ROLL LEFT 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE.

MAP REVIEW

77:08

MCC -H ti

LMP

CMP

CDR

2/150/B&W, 1/250 F 2.8 77:14

P22 MANUAL ACQ SA 0°, TA 10° EAT PERIOD

BEGIN REV 5

I CNTL POINT SIGHTING IP I ACQ

77:30

2/150/B&W, 1/250 (CDR) PITCH DWN AT 0.3°/SEC AT ACQ

CP2 NO. 526 LAT -10.200°S LONG/2 +77.550 ° +000.00 ALT nm NEW COORDINATES LAT LONG/2 ALT

77:44

ACQUIRE S/C

nm ACQUIRE MSFN ON OMNIS AT LOSS PITCH UP AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE.

REST PERIOD (3 HOURS)

REPORT NEW CP COORDINATES

REVIEW LDMK MAP

78:00 MISSION

EDITION

DATE

TIME

AS503/103

FINAL

November 22, 1968

77:00 - 78:00

MSC Form 1910 (Nov 88)

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

4/LPO

2-59

FLIGHT PLAN LMP

CMP •

CDR

MCC—H 6

PSEUDO LDG SITE SIGHTINGS P22 - AUTO OPTICS IPI TCA LDMK NO, 81 LAT +02.675°N LONG/2 +17.512° -000.99 nm ALT NEW COORDINATES LAT + LONG/2 + ALT

PITCH DWN 0.3°/SEC AT ACQ AT LOSS ROLL RIGHT 180° AT 2°/SEC TO HEADS DWN GO INERTIAL

0

n

V64 ACQUIRE MSFN ON HGA 1/80/HS, 1/4, F 2.8

ACQUIRE S/C P27 UPDATE: STATE VECTOR VOICE UPDATE: BLOCK DATA MAP_ UPDATE 5/6

REPORT NEW COORDINATES RECORD BLOCK DATA (TEI 6 ), & MAP UPDATE

REST PERIOD (3 HOURS) IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF --

VERIFY SYSTEMS STATUS

DUMP DSE

TORQUE ANGLES: X

zY

. GDC ALIGN TO IMU 16/18/ C EX, 1/250, 1 fps MAGS) 2/150/C121/1/250 SPOT GENERAL OBSERVATIONS a

MISSION

AS503/103 MSC Form 1910 (Nov 68)

•

0

EDITION

FINAL

DATE

Novemb e r 22, 1968

TIME

78:00 - 79:00

DAY/REV

4/LPO

PAGE

2-60

FLIGHT PLAN

ti

•

•1

0 0

0

FLIGHT PLAN MCC—H S

LMP

CMP

CDR

REVIEW CONTROL POINT MAP ROLL 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE

!CNTL POINT SIGHTING]

REST PERIOD (3 HOURS)

P22 - AUTO OPTICS IPI TCA CP2 NO. 526 LAT -10.200°S LONG/2 +77.550° ALT

+000.00 nm

NEW COORDINATES LAT LONG/2 ALT

PITCH DWN 0.3°/SEC AT AC 0 nm

T LOSS PITCH UP AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE

REVIEW LDMK MAP

CQUIRE MSFN ON OMNIS

ACQUIRE S/C

REPORT NEW COORDINATES

'PSEUDO LDG

SITE SIGHTING!

•

MISSION

AS503/103 MSC Form 1910 (Nov Ea)

EDITION

FINAL

TIME

DATE

November 22, 1968

79:.00 - 80:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

4/LPO

2-61

FLIGHT PLAN CMP

CDR

80:00

LPAP

P22 AUTO OPTICS IPII TCAI LDMK NO. B1 LAT +02.675°N LONG/2 +17.512° -000.99 nm ALT NEW COORDINATES LAT LONG/2 ALT

80:13

0:19

PITCH DWN 0.3°/SEC AT ACQ

0 nm

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , STAR ANGLE DIFF

2/150/B&W, 1/250 (R&B) TRANS TO RIGHT COUCH

TORQUE ANGLET— -Xy

MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 88)

•

0

AT LOSS ROLL RIGHT 180° AT 2°/SEC. GO INERTIAL V64 ACQUIRE MSFN ON HGA ACQUIRE S/C P27 UPDATE: STATE REPORT NEW COORDINATES VECTOR RECORD BLOCK DATA VOICE (TEI 7 )& MAP UPDATE UPDATE: BLOCK DATA & MAP UPDATE 6/7 VERIFY SYSTEMS STATUS DUMP DSE 1/80/B&W, 1/250 F 2.8 IN

REST PERIOD (3 HOURS)

ROLL LEFT 180° AT 2°/SEC PITCH UP AT 0.2°/SEC TO BEGIN ORDEAL 0, 5, O. ORB RATE

MCC—H

•

EAT PERIOD 16/SXT/NEW C XT, 6 fps

TIME

DATE

November 22, 1968

80:00 - 81:00

FLIGHT PLANNING

DAY/REV

PAGE

f

2-62

4/LPO

H

14 ,

0 •

0 • FLIGHT PLAN 81:00 --

MCC—H

LMP

CMP

CDR

BIOMED Sw - LEFT

ICNTL PT SIGHTINGS (3)1 81:05-

81:11 -

P22 MAN ACQ SA 0° TA 10° IPI PITCH DWN AT 0.3°/SEC AT ACQ ACQ CP1 NO. 504 ---05.250°S LAT AT LOSS PITCH UP AT LONG/2 -81.350° 0.5°/SEC TO +000.00 nm ALT ORDEAL 0, 5, 0

EAT PERIOD

NEW COORDINATES LAT LONG/2 ALT EAT PERIOD NEW COORDINATES LAT LONG/2 ALT

P22 MAN ACQ SA 0° TA 10° IPI I ACQ I .• NEW COORDINATES CP3 NO. 334 -09.100°S LAT PITCH OWN AT 0.3°/SEC AT LAT . LONG/2 +47.950° LONG/2 CQ +000.00 nm ALT ALT

nm

ACQUIRE 5/C °

nm

'PSEUDO LOG SITE SIGHTING' P22 AUTO OPTICS

MISSION

EDITION

DATE

AS503/103

FINAL

November 22, 1968

MSC Form 1910 (Nov 68)

nm

T

P22 AUTO OPTICS IPI I -TCA 1 ' PITCH DWN AT 0.3°/SEC AT CP2 NO. 526 -10.200°S ACQ LAT LONG/2 +77.550 ° +000.00 nm ALT T LOSS PITCH UP AT 0.5°/SEC TO RDEAL 0, 5, 0

AT LOSS PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0

0

FUG

TIME

81:00 - 82:00

DAY/REV

PAGE

4/LPO

2-63

FLIGHT PLAN CMP •

82:00 —

PITCH DWN AT 0.3°/SEC AT ACQ 82:11 AT LOSS ROLL RIGHT 180° AT 2°/SEC GO INERTIAL ACQUIRE MSFN ON HGA

82:17

LMP

IP I TCA LDG SITE NO. B1 LAT +02.675°N LONG/2 +17.512° ALT -000.99 nm NEW COORDINATES LAT LONG/2 ALT

MCC—H

0

nm

REPORT NEW COORDINATES RECORD MAP UPDATE & BLOCK DATA (TEI 8 ) REST PERIOD (2 HOURS)

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE JIF!F --

82:30 —

ACQUIRE S/C P27 UPDATE: STATE VECTOR VOICE UPDATE: MAP UPDATE 8 BLOCK DATA DUMP DSE

TORQUE ANGLES: X Y Z GDC ALIGN TO IMU

82:53

83:00

— I

•

ROLL LEFT 180° AT 2°/SEC TO HEADS UP

16/SXT/CXT„6 fps

I

MISSION

AS503/103, MSC Form 1910 (Nov 08)

0 0

EDITION

FINAL

DATE

November 22, 1968

TIME

82:00 - 83:00

DAY/REV

4/LPO

PAGE

2-64

FLIGHT PLANNI

0

0

0 •

•

0

FLIGHT PLAN PITCH DWN AT. 0.2°/SEC TO ICNTL PT SIG}-TINGS (3) ORDEAL 0, 5, 0 P22 AUTO OPTICS 11)1 __. .._, __ __ TCA CP1 NO. 504 LAT -05.250°S LONG/2 -81.350° PITCH DWN AT 0.3°/SEC ALT +000.00 nm AT ACQ

83:03

83:10

P22 AUTO OPTICS IPI

AT LOSS PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0

EGIN REV 8

TCA

PITCH OWN AT 0.3°/SEC AT ACQ

83:30

MCC-H ti

LMP

CMP

CDR

3:00

REST PERIOD (2 HOURS) NEW COORDINATES LAT LONG/2 ALT

nm

. •

.

CP2 NO. 526 LAT -10.200 ° S LONG/2 +77.550° +000.00 nm ALT

NEW COORDINATES LAT LONG/2 ALT

0 nm

PITCH UP AT 0.5 ° /SEC TO ORDEAL 0, 5, 0

83:39 ACQUIRE MSFN ON OMNIS . PITCH OWN AT 0.3°/SEC AT ACQ

P22 AUTO OPTICS IPII TCA • CP3 NO. 334 LAT • -09.100°S LONG/2 +47.950 ° +000.00 nm ALT

ACQUIRE S/C NEW COORDINATES LAT LONG/2 ALT

0

nm

PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0

PSEUDO LOG SITE SIGHTINGI

•

P22 AUTO OPTICS

84:00 MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

TIME

DATE

November 22, 1968

83:00 - 84:00

FLIGHT PLANNING BRANCH

DAY, REV

4/LPO

PAGE

2-65

FLIGHT PLAN 84:0

IPI

PITCH DWN AT 0.3°/SEC AT ACQ 84:10 AT LOSS ROLL RIGHT 180° AT 2°/SEC (HEADS DWN) GO INERTIAL ACQUIRE MSFN ON HGA

84:16

I

CMP •

TCA LDMK NO. 81 LAT +02.512°N LONG/2 +17.512° ALT +000.99 nm

NEW COORDINATES LAT LONG/2 ALT

I

nm

REST PERIOD (2 HOURS)

1

LION CANISTER CHANGE (CARTRIDGE 10 FROM B5 INTO CANISTER B)

ACQUIRE S/C

2/150/NEW B&W, 1/250 (R&B)

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , _ STAR ANGLE DIFF

84:30 —

MCC—H

LMP

BIOMED Sw - RIGHT

P27 UPDATE: STATE VECTOR

VERIFY SYSTEMS STATUS

DUMP DSE VOICE UPDATE: MAP UPDATE 8/9 BLOCK DATA

TORQUE ANGLES: X RECORD MAP UPDATE & BLOCK DATA (TEI 9 )

z DC ALIGN PITCH UP AT 0.2°/SEC TO ORDEAL 180, 0, 0 (HEADS DWN) BEGIN ORB RATE

84:51

1/80/H.S. B, f2.8, POL REST PERIOD (2 HOURS)

SR -12 MIN START DARK 1/80 B&W, 1/4, f4,POL

16/18/NEW CEX, 1/250, f2.8, 1 fps

85: 00 -I

•

•

MISSION

I DITION

AS503/103

FINAL

MSC Form 1910 (Nov 58)

•

SR -4 MIN START CORONA

0

TIME

DATE

November 22, 1968

84:00 - 85:00

DAY/REV

4/LPO

FLIGHT PLANNING BRANCH

0

PAGE

2-66

•

,4r

FLIGHT PL AN AT S/C SR PITCH UP 60° AT 0.5°/SEC` TO ORDEAL 180, 300, 0 CONTINUE ORB RATE START CAMERA AT S/C SR +12 MIN

85:08

MCC—H •

LMP •

CMP •

CDR

85:00 85:0

1/80/NEW C BRKT INT

START CAMERA I AT SR +12 MIN

ZERO PHASE TARGETS OF OPPORTUNITY

BEGIN REV 9

CONVERGENT STEREO PHOTOGRAPHY-EXTRA EXP EACH 5 MIN NITE TIME

85:30 REST PERIOD

85:3

(2 HOURS)

PITCH UP 40° AT 0.2°/SEC TO ORDEAL 180, 260, 0

ACQUIRE MSFN ON HGA

ACQUIRE S/C

RECORD MAP UPDATE

VOICE UPDATE:

MAP UPDATE 9/10

]

ROLL RT AS REQD TO SHADE WINDOWS-KEEP X-AXIS +10° ON TRACK 2/80 B&W/R&B

TV

4 STOPS WIDER

86: 00 TIME

MISSION

EDITION

DATE

AS503/103

FINAL

November 22, 1968

MSC Farm 1910 No

6 8)

FLIGHT PL

N I

85:00 - 86:00

DAY/REV

PAGE

4/LF0

2-67

FLIGHT PLAN CMP

CDR •

LMP

MCC—H

I

ri

REST PERIOD (2 HOURS)

STOP CAMERA AT TERM

STOP CAMERA AT TERM 2/80/HS, 1/4 f2.8

ROLL RIGHT 180° IF REQD PITCH DWN 60° AT 0.2°/SEC TO ORDEAL 180, 310, 0 (HEADS DWN) GO INERTIAL

P27 UPDATE: STATE VECTOR RECORD BLOCK DATA (TEI 10 ) & MNVR PAD

VOICE UPDATE: BLOCK DATA MNVR PAD DUMP DSE

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST , STAR ID STAR ANGLE DIFF

VERIFY SYSTEMS STATUS

TORQUE ANGLEST----x Y PITCH DWN AT 0.2°/SEC TO ORDEAL 180, 180, 0 BEGIN ORB RATE (HEADS DWN +Z FWD)

1/80/NEW B&W 1/250, f2.8 INT (CDR) 2/150/C, 1/250

• MISSION

EDITION

DATE

AS503/103

FINAL

i November 22, 1968

MSC Form 1910 (Nov 68)

TIME

86:00 - 87:00

DAY/REV

PAGE

4/LPO

2-58

FLIGHT PLANNING BRANCH

0

0

I

• FLIGHT PLAN MCC—H •

LMP

CMP

CDR

•

MNVR TO TEI ATT SXT STAR CK PITCH UP AT 0.2°/SEC TO ORDEAL 180, 180, 0 BEGIN ORB RATE

BEGIN REV 10

EAT PERIOD

EAT PERIOD

EAT PERIOD

2/150/B&W OR 0,1/250 ACQUIRE MSFN ON HGA

ACQUIRE S/C

RECORD MNVR PAD, BLOCK DATA (TEI 11 ), MAP UPDATE

-

MISSION

AS503/103 MSC Form 1910 (Nov 68)

EDITION

FINAL

TIME

DATE

November 22, 1968

87:00 - 88:00

FLIGHT PLANNING BRANCH

DUMP DSE PIPA BIAS CK P27 UPDATE: STATE VECTOR TARGET LOAD VOICE UPDATE:

MNVR PAD BLOCK DATA

1'

MAP UPDATE 10

DAY/REV

PAGE

4/LPO

2-69

FLIGHT PLAN CMP •

CDR

88:00 —

LMP

MCC—H

BIOMED Sw - GO/NO GO LEFT

GO/NO GO FOR TEI

88:07 88:13 2/150/C SPOT 16/75/CEX/1 fps/SPOT

IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF

PRE TEI SYSTEMS CKS C&W CK CM RCS CK SM RCS CK SPS PERIODIC MONITOR EPS PERIODIC MONITOR ECS PERIODIC MONITOR

TORQUE AGES

Y

88:30 — EXTERNAL AV P30 EMS TEST SPS THRUST P40 MNVR TO BURN ATT

PUGS MODE Sw - AUX

MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

• •

SXT STAR CK TRANSFER TO COUCH

TIME

DATE

November 22, 1968

88:00 - 89:00

DAY/REV

_

4/LPO

PAGE

2-70

FLIGHT PLANNING BRANCH

(4

0

0 TEI BURN CHART

BURN STATUS REPORT X I X X X

ATIG BT •t

T RIM >XXi 1 XI X X )()0 !

V gx

IY

REMARKS:

10 ° /SEC TAKEOVER

2850-950

gx

V gY T-V gz C

X XIX X X A Xti 'X X:Xi

TEl

ATT DEVIATION 10° TAKEOVER

SHUTDOWN TIME B/T+2 SEC & AV -40 fps c

RESIDUALS TRIM TO 2,0 fps

TEI ABORT MODES-SYSTEMS PROBLEMS:15-MIN ABORT CHART OTHERWISE TEI V qo B/T ABORT MODE TRAJECTORY V

t

P or Y RATES

FUEL . !Ox - 'UNBALANCE

950-600 600-0

0 -2:00 LUNAR ORBIT MODE III AFTER 1 REV 2:00-2:20 UNSTABLE 5-HR COAST, MODE I 2:20-2:54 HYPERBOLIC COAST OUT OF SPHERE - P37

FLIGHT PLAN CMP •

CDR •

89 : 0 0

LMP

MCC—H

•

SM RCS MON CK GETI = 89:15:07 AV = 3532 fps BT = 3, MIN 26 SEC

GDC ALIGN TO IMU

iTEII

89:76 -

SM RCS MON CK

PITCH UP TO VERTICAL +Z FWD) TO ACQ MOON

SPS MON CK

IN WIND W

ACQUIRE MSFN WITH HGA

CDR CREW STATUS REPORT TRANS CSM STATE VECTOR TO LM SLOT 89:30 —

SLEEP PERIOD (5 HOURS)

ml

REINITIALIZE W MATRIX R +00094 1 R 2 +00571 R 3 +00003

ACQUIRE S/C

TEI BURN STATUS REPORT

INITIATE BAT CHARGE BIOMED Sw - CENTER

89:45 -

I

DUMP DSE UPDATE ENTRY REFSMMAT •

•

90:00 :I MISSION

AS503/103,

EDITION

FINAL

DATE

TIME

November 22, 1968

•

89:00 - 90:00

DAY/ REV

4/TEC

PAGE

2-71

FLIGHT PLANNING BRANCH

MSC Form 1310 (Nov 68)

4I)

4D 0

0

0 • FLIGHT PLAN

MCC— H

LMP •

LMP •

CDR

90:00 --

MNVR TO P52 ATT IMU REALIGN P52 OPTION 1 - PREFERRED STAR ID STAR ANGLE DIF — 90:15-

TORQUE ANGLET- -X

90:30

SLEEP PERIOD (5 HOURS)

TRN BIAS MNVR TO SIGHTING ATT

LCISLUNAR NAVIGATION P231 1. STAR 01 LNH L H STAR 2 SETS — 90:45 -

2. STAR 02 LNH STAR L H

•

•

91:00 --

, MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

TIME

90:00 - 91:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

4/TEC

2-72

FLIGHT PLAN

.

CMP

CDR

MCC—H

LMP

91:00

91:15

TRN BIAS MNVR TO SIGHTING ATT 3.

STAR 10 LFH STAR L

H

2 SETS 91:30

F

SLEEP PERIOD (5 HOURS)

4. STAR 11 LFH STAR

L

H

2 SETS

91:45

92:00 MISSION

AS503/103 MSC Form 1910 (Nov 08)

EDITION

FINAL

TIME

DATE

November 22,1968

91:00 - 92:00

DAY/REV

4/TEC

PAGE

2-73

FLIGHT PLANNING BRANCH

0

•

0

0

FLIGHT PL AN e•-11L—i

MCC—H I

LMP •

OAP •

CDR

92:00

MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0,1°/SEC

92:15

S

92:30

F

SLEEP PERIOD (5 HOURS)

92:45

93:0

i MISSION

AS503/103 MSC Form 1910 (Nov 69)

EDITION

FINAL

TIME

DATE

November 22,1968

92:00 - 93:00

FLIGHT PLANNING BRANCH

DAY/REY

PAGE

4/TEC

2-74

FLIGHT PLAN CDR

CMP

MCC—H

CMP

93: 00—

SLEEP PERIOD (5 HOURS)

93:30 -

EAT PERIOD

EAT PERIOD

BIOMED Sw LEFT CMP/LMP CREW STATUS REPORT

MIR

94:00 —

94:30 -

95:00

EAT PERIOD

SLEEP PERIOD (7 HOURS)

]

MISSION

EDITION

AS503/103

FINAL

MSC Farm 1910 (Nov BB)

•

SLEEP PERIOD (5 HOURS)

0

TIME

DATE

November 22, 1968

93:00 - 95:00

DAY/REV

4/TEC

PAGE

2-75

FLIGHT PLANNING BRANCH

•

0 0

•

0

'0

0

FLIGHT PLAN 95:00_

CDR •

•

CMP

thiP

MCC—H I

CDR CREW STATUS REPORT

95:15 -

95:30

SLEEP PERIOD (5 HOURS)

S F

—

SLEEP PERIOD (5 HOURS)

N

95:45 -

LiOH CANISTER CHANGE (CARTRIDGE NO. 10 FROM B5 INTO CANISTER B)

MNVR TO P52 ATT 96:00-MISSION

EDITION

DATE

TIME

AS503/103

FINAL

November 22, 1968

95:00 - 96:00

MSC Farm 1918 (Nov 68)

FLIGHT PLANNING BRANCH

DAY/REV

4/TEC

PAGE

2-76

FLIGHT PLAN CDR

LMP

CMP

MCC-H

I

96: 00 — IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DI FF --TORQUE ANGLES: X

Y

96:75

MNVR TO PTC ATT P 029 Y 315 ROLL 0.17TEC

SLEEP PERIOD (5 HOURS)

96:30 —

SLEEP PERIOD (5 HOURS)

96:45 —

97:00

:1

I MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov E8)

0

TIME

DATE

November 22, 1968

96:00 - 97:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-77

• •

•

0 0

FLIGHT PLAN CDR

MCC—H

LMP

C MP

97: 00—

97:30 -

SLEEP PERIOD (5 HOURS)

98:00_

F N

SLEEP PERIOD (5 HOURS)

98:30 -

99:00

•

•

MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

TIME

DATE

November 22,

1968

97:00 - 99:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-78

FLIGHT PL AN CMP

CDR

LMP

MCC—H

99:00 —

BIOMED Sw -,C ENTER

99:15 -

99:30 —

EAT PERIOD

EAT PERIOD

I

EAT PERIOD

1=1

99:45 -

100:00

•

MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

0

DATE

November 22,

TIME

1968

99:00 - 100:00

DAY/ REV

5/TEC

PAGE

2-79

FLIGHT PLANNING BRANCH

0

•••

0 0 FLIGHT PLAN

100:00

MNVR TO P52 ATT

MCC—H

LMP

CMP

CDR

CMP/LMP CREW STATUS REPORT

IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF TORQUE ANGLES: X

100:15

MNVR TO SIGHTING ATT

TRN BIAS LCISLUNAR NAVIGATION P231 1. STAR 02 LNH STAR L H -1 SET

100:30

2.

STAR 11 STAR 1 SET

LFH L

H

100:45 STAR 01 LNH L STAR 1 SET

3.

H

MNVR TO SIGHTING ATT

•

10 1 :00 MISSION

S503 103 MSC Form 1910 (Nov 68)

EDITION

DATE

TIME

FINAL

November 22, 1968

100:00 - 101:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

5/TEC

2-80

FLIGHT PLAN CMP

CDR

IMP •

101:00

•

MCC—H

101:15

TRN BIAS

CISLUNAR NAVIGATION P23 STAR 22 EFH STAR E H 2 SETS

101:30

• STAR 26 ENH STAR E 101 :45

H

2 SETS

BIOMED Sw - RIGHT 102:00

a

MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 00)

0

TIME

DATE

November 22, 1968

101:00 - 102:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

5/TEC

2-81

0 0

0 FLIGHT PL AN

MCC—H

LMP

CMP

CDR

I

102:00 3.

STAR 31 ENH STARE 2 SETS --

H

102:15

P27 UPDATE STATE VECTOR TGT LOAD REFSMMAT

102:30

MNVR TO P52 ATT

VOICE UPDATE: MNVR PAD

RECORD MNVR PAD IMU REALIGN P52 OPTION 3 - RESFMMAT STAR ID STAR ANGLE DI FF-

102:45

TORQLTE ANGUE-S. .-- -X

103:00 MISSION

EDITION

AS503/103

FINAL

MSC Form 1919 (Nov ES)

DATE

November 22, 1968 FLIGHT

TIME

102:00 103:00

DAY/REV

PAGE

5/TEC

2-82

MCC ' S

BURN STATUS REPORT

X

X

X

X

---- 7TRIM X X X

BURN CHART

tTIG ,BT V gx

P or Y RATES

ATT DEVIATION

SHUTDOWN TIME

10° TAKEOVER

B/T +1

RESIDUALS

_ MCC(ALL) 10°/SEC TAKEOVER

R

P

X X X

SEC

TRIM TO 0.2 fos

'XXX

V ....+ _.

;\) 1 co I.)

V

gx gY

v gz

P

AV C

X X X

FUEL

X X X

Ox

X X X

UNBALANCE

REMARKS:

0 0

•

•

•

0

0 0

FLIGHT PLAN ,

103:15

MCC —H

LMP •

CMP •

CDR

103:00

I

V47 TRANS LM STATE VECTOR TO CSM SLOT EXT hV P30 SPS/RCS THRUST P40/41

103:30 MNVR TO BURN ATT SXT STAR CK

103:45

EMS TEST

TEI+15

GDC ALIGN TO IMU 1CT 5 0.--- NOMINALLY ZERO

PIPA BIAS CK

TRANS TO COUCH

SM RCS MON CK

104:00

, MISSION

AS503/103 MSC Form 1210 (Nov 68)

EDITION

FINAL

TIME

DATE

November 22, 1968

103:00 - 104:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-83

FLIGHT PLAN CDR

•

104:00 --

CMP

V66 TRANS CSM STATE VECTOR TO LM SLOT

MCC-11

LMP

MCC 5 BURN STATUS REPORT INITIATE BAT CHARGE

SM RCS MON CK

I

UNSTOW TV CAMERA

104:15 — TV

104:30 —

EAT PERIOD

F

EAT PERIOD

EAT PERIOD

.l-

N

STOW TV CAMERA

104:45 —

CDR CREW STf TUS REPORT 105:00 —1 MISSION

EDITION

DATE

AS503/103

FINAL

November 22 1968

MSC Form 1910 (Nov 68)

•

TIME

104:00 - 105:11

DAY/REV

PAGE

1111/111111111/111111

FLIGHT PLANNING BRANCH

0 0

0 0

0 FLIGHT PLAN •

105:00--

LiOH CANISTER CHANGE (CARTRIDGE NO. 12 FROM B6 INTO CANISTER 13)

105:15 -

MCC—H

LMP •

crow

CDR

6

BIOMED Sw - CENTER TRANS TO LH COUCH MNVR TO SIGHTING ATT

TRN BIAS CISLUNAR NAVIGATION P23 1.

STAR 22 EFH E H STAR 2 SETS

M 105:30 —

S F

N

SLEEP PERIOD (7 HOURS)

2. STAR 26 ENH STAR E H 1 SET 105:45 -

STAR 31 ENH STAR E H 2 SETS

3.

•

106:00-MISSION

EDITION

AS503/103

FINAL

MSC Form 1610 (Nov 68)

TIME

DATE

November 22, 1968

105:00 - 106:00

FLIGHT PLANNING

N

DAY/REV

PAGE

5/TEC

2-85

FLIGHT PLAN LMP •

CMP •

CDR

106:00

MCC —H

S

MNVR TO SIGHTING ATT

TRN BIAS STAR 02 LNH STAR L 1 SET

1.

106:15

STAR 11 LEH STAR L

2. 106:30

S

F

SLEEP PERIOD (7 HOURS)

H

H

1 SET

N 3.

STAR 01 LNH STAR L

H

1 SET 106:45 RETURN TO EARTH P37

107:00-1 MISSION

EDITION

AS503/103

FINAL

MSC Form i9:0 (Nov 68)

0 0

DATE

November 22, 1968

TIME

106:00 - 107:00

DAY/REV

5/TEC

PAGE

2-86

FLIGHT PLANNI

0 0

•

•

41

0

I

.

FLIGHT PLAN MCC—H •

LIMP

CDR

107:00

107:15

107:30

S

F

N

SLEEP PERIOD (7 HOURS)

MNVR TO P52 ATTITUDE

IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DEFT 1 07:45

TORQUE ANGLES:

MNVR TO SIGHTING ATT

•

108:00 MISSION

EDITION

DATE

AS503/103

FINAL.

November 22,1968

MSC Form 191O (Nov 68)

TIME

107:00 - 108:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-87

FLIGHT PLAN CMP •

CDR

108:00 --

LMP •

MCC—H •

CISLUNAR NAVIGATION P231 BIOMED Sw - RIGHT 1.

STAR 22 EFH STAR E H 1 SET

2.

STAR 26 ENH STAR E 2 SETS --

3.

STAR 31 ENH STAR E H 2 SETS

108:15 -

1

108: 30—

SLEEP PERIOD (7 HOURS)

-I

MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1°/SEC P&Y FREE REESTABLISH PTC AT +15° IN P OR Y AND RECORD GET

108:45

RETURN TO EARTH P37

109:00 :1 MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 08)

9 0

TIME

DATE

November 22,1968

108:00 - 109:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-88

•

0

FLIGHT PLAN MCC—H •

LMP •

CMP

CDR

109:00

109:30

H S 1 10:0 0

F N

SLEEP PERIOD (7 HOURS)

110: 3 0

•

•

111:00 MISSION

AS503/103 MSC FLIrm 1910 (Nov 6$)

EDITION

FINAL

TIME

DATE

November 22,1968

109:00

- 111:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

5/TEC

2-89

FLIGHT PLAN CDR

CMP

LMP

MCC— H

111:00

SLEEP PERIOD (7 HOURS)

111:30

EAT PERIOD

I

EAT PERIOD

CMP/LMP CREW STATUS REPORT BIOMED Sw - LEFT 112:00

EAT PERIOD

112:30

113:00

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

-I MISSION

AS503/103 MSC Form 1910 (Nov 58)

EDITION

FINAL

TIME

DATE

November 22,

196e

111:00 - 113:00

DAY/ L

Inv

5/TEC

PAGE

2-90

FLIGHT PLANNING BRANCH

0 0

•

0

• 4• FLIGHT PLAN MCC-H

LMP

CMP

CDR

f

113:00

CDR CREW STATUS REPORT 113:30 -

.M1

114:00 —

S

SLEEP PERIOD (7 HOURS)

F N

SLEEP PERIOD (7 HOURS)

114:30

.=1

MNVR TO P52 ATT

•

115:00 MISSION

EDITION

AS503/103

FINAL

MSC Form 19:0 (Nov 68)

TIME

DATE

November 22, 1968

113:00 - 115:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-91

FLIGHT PLAN CDR

CMP

L PAP

MCC—H 4

115:00 IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF TORQUE ANGLES: X Y

115:15

MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1 °/SEC SLEEP PERIOD (7 HOURS)

115:30

SLEEP PERIOD (7 HOURS)

115:45

116:00

i MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

• 0

TIME

115:00 - 116:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-92

•

0 0

•

FLIGHT PL AN CDR

CMP

LMP

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

MCC-H

116:00

116:30

117:00

117:30

•

118:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 66)

TIME

116:00 - 118:00

FLIGHT PLANNING BRANCH

DAY/REV

5/TEC

PAGE

2-93

FLIGHT PLAN 118:00 —

EAT PERIOD

118:30 -

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

LiOH CANISTER CHANGE (CARTRIDGE NO. 13 FROM B6 INTO CANISTER A)

M S 119:00 —

MCC ..-14 S

L MP

CMP

CDR

•

F

BIOMED S - CENTER

N

119:30 —

EAT PERIOD

EAT PERIOD

1 MNVR TO SIGHTING ATT

TRN BIAS

•

120:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

•

MSC Form 1910 (Nov 68)

0

TIME

118:00 - 120:00

DAY/REV

PAGE

5/TEC

2-94

FLIGHT PLANNING BRANCH

0 0

FLIGHT PLAN •

CISLUNAR NAVIGATION P23 .

STAR 22 EFH STARE 1 SET -

CMP/LMP CREW STATUS REPORT

H

.

STAR 26 ENH STAR E H — 1 SET

.

STAR 31 ENH STAR E H — 1 SE 7-

120:15 -

MCC—H •

LMP •

CMP

CDR

120:00 -

120:30

120:45 -

RECORD MNVR PAD

P27 UPDATE: STATE VECTOR TOT LOAD VOICE UPDATE: MNVR PAD

121:00 -MISSION

EDITION

AS503/103

FINAL

MSC Form 1919 (Nov 98)

TIME

DATE

November 22, 1968

120:00 - 121:00

FLIGHT PLANNING BRANCH

DAY/REV

6/TEC

PAGE

2-95

MCC'S

BURN STATUS REPORT X

•

X

XX

BURN CHART

_ATIG

•

BT V gx

TRIM. XXX

R

XXX

P

X XX

Y V V

V

c)

P or V RATES MCC(ALL) 10°/SEC TAKEOVER

ATT DEVIATION

SHUTDOWN TIME

10° TAKEOVER

B/T +1

SEC

RESIDUALS TRIM TO 0.2 fns

gx gY

9.2 AV c

X X X

FUEL

X

X

X

Ox

X X

X

UNBALANCE

REMARKS:

•

0

'

0 • FLIGHT PL AN

MCC—H •

LMF

CMP •

CDR •

121:00

MNVR TO P52 ATT IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF -121:15

ToRqUT ANGLET— -X Y

Z V47 TRANS LM STATE VECTOR TO CSM SLOT EXT AV P30 121:30 SPS/RCS THRUST P40/41 MNVR TO BURN ATT

SXT STAR CK 121:45

TEI f 33 HRS

EMS TEST

TRANS TO COUCH

GDC ALIGN MCC 6 ❑ V=NOMINALLY ZERO

SM RCS MON CK

PIPA BIAS CK

•

122:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSG Form 1810 (Nov 68)

TIME

121:00 - 122:00

FLIGHT PLANNING BRANCH

DAY/REV

6/TEC

PAGE

2-96

FLIGHT PLAN CDR

CMP

MCC—H

LMP

I

122:00 V66 TRANS CSM STATE VECTOR TO LM SLOT

SM RCS MON CK

MCC 6 BURN STATUS REPORT INITIATE BAT CHARGE

STONED Sw - RIGHT 122:15

MNVR TO SIGHTING ATT

122:30

TRN BIAS

1CISLUNAR NAVIGATION P231 1.

STAR 02 LNH STAR L H 2 SETS

2.

STAR 01 LNH STAR L H 1 SET

122:45

I

123:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

TIME

122:00 - 123:00

DAY/REV

6/TEC

PAGE

2-97

FLIGHT PLANNING BRANCH

0

0 FLIGHT PLAN 123:00

MCC—H

OAP •

CMP •

CDR

RETURN TO EARTH P37 MNVR TO SIGHTING ATT

123:30

123:30

F N TRN BIAS [CISLUNAR NAVIGATION P23 1.

STAR 22 EFH STAR E H 2 SETS —

2.

STAR 26 ENH E STAR 1 SET

123:45

124:00 MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

H • TIME

DATE

November 22, 1968

1

123:00 - 124:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

6/TEC

2-98

FLIGHT PLAN CMP

CDR

1MP

124:00 —,

MCC—H

STAR 31 ENH STAR E H 2 SETS —

124:15 -

MNVR TO PTC ATT P 029 Y 315

124:30

RETURN TO EARTH P37

ROLL 0.17 EC

124:45 -

125:00-1 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

•

0

TIME

•

124:00 - 125:00

DAY/REV

6/TEC

PAGE

2-99

FLIGHT PLANNING BRANCH

0 0

•

• •

0 FLIGHT PLAN

MCC—H •

LMP

CMP

CDR •

•

125:00 --

BIOMED Sw - CENTER

125:30 -

M S F

126:00 —

N

126:30 -

EAT PERIOD

EAT PERIOD

EAT PERIOD

CDR CREW STATUS REPORT 4

6

127:00 -MISSION

EDITION

AS503/103

FINAL

MSC Form 1910 (Nov 68)

TIME

DATE

November 22,1968

125:00 - 127:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

6/TEC

2-100

FLIGHT PLAN LMP

CMP

CDR

MCC—H

127:00 — LiOH CANISTER CHANGE (CARTRIDGE NO. 14 FROM B6 INTO CANISTER B)

127:30 11.

BIOMED Sw - RIGHT UNSTOW TV CAMERA SLEEP PERIOD (7 HOURS)

128:00 —

TV

.m1

STOW TV CAMERA 128:30 —

i 129:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1610 (Nov 68)

TIME

127:00 - 129:00

DAY/REV

PAGE

6/TEC

2-101

FLIGHT PLANNING BRANCH

0 0

0 FLIGHT PLAN 129:00 —

•

MCC —H

LMP

CMP •

CDR

•

I

129:15 -

M 129:30 —

S F N

SLEEP PERIOD (7 HOURS) MNVR TO P52 ATT

IMU REALIGN P52 OPTION 3 - REFSMMAT , STAR ID STAR ANGLE 15-I-FF -129:45 -

TORQUE ANGLE S : X Y

MNVR TO SIGHTING ATT

TRN BIAS

•

130:00-- •

MSC

MISSION

EDITION

AS503/103

FINAL

Form 1910 (Nov 68)

TIME

DATE

November 22,1968

129:00 - 130:00

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DAY/REV

PAGE

6/TEC

2-102

FLIGHT PLAN CMP •

CDR

130:00 —

MCC—H

LMP

CISLUNAR NAVIGATION P23 ' STAR 02 LNH STAR_ 2 SETS —

H

130:15 -

S 130:30 —

F N

SLEEP PERIOD (7 HOURS)

MNVR TO SIGHTING ATT

TRN BIAS

130:45 —

.

STAR 22 EFH STAR E 2 SETS

H

S

131:00 MISSION

AS503/103 MSC Forin 1910

•

(NoV $8)

EDITION

FINAL

TIME

DATE

November 22,

1968

130:00

-

131:00

DAY/REV

6/TEC

PAGE

2-103

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0

0

0 0 FLIGHT PLAN MCC-H

LMP

CMP

CDR

6

131 :00 BIOMES Sw - CENTER

2.

STAR 26 ENH E H STAR 2 SETS

3.

STAR 31 ENH STARE H 2 SETS --

131 :15

131 :30

S F

N

SLEEP PERIOD (7 HOURS)

131:45

MNVR TO PTC ATT P 029 Y 315

P RETURN TO EARTH P37 132:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

TIME

131:00 - 132:00

FLIGHT PLANNING BRANCH

Y

ROLL 0.1°/SEC • DAY/REV

6/TEC

PAGE

2-104

FLIGHT PLAN CDR

CMP

LMP

MCC—H

132:00

EI -15 HRS P27 UPDATE: STATE VECTOR GO/NO GO VOICE UPDATE: BLOCK DATA FOR EI -2 HOURS MCC .

STATE VECTOR GO/NO GO RECORD BLOCK DATA FOR EI -2 HOURS 13230

SLEEP PERIOD (7 HOURS)

133:00

EAT PERIOD

133:30

EAT PERIOD

I

CMP/LMP CREW STATUS REPORT

_

BIOMED Sw - LEFT 1 3 4:00 -1 MISSION

AS503/103 11SC Form 1910 (Nov 68)

• 0

EDITION

FINAL

DATE

November 22,1968

TIME

132:00 - 134:00

DAY/REV

6/TEC

PAGE

2-10 5

FLIGHT PLANNING BRANCH

0 e0

• •

•

4;

FLIGHT PL AN MCC- H

LMP

CMP

CDR

134:00

134:15

134:30

EAT PERIOD

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

134:45

•

135:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

TIME

134:00 - 135:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

6/TEC

2-106

FLIGHT PLAN CMP

CDR

135:00

•

LMP

MCC—H

BEGIN CABIN COLD SOAK CDR CREW STATUS REPORT

135:15 -

MNVR TO P52 ATT 1

135:30 —

SLEEP PERIOD (7 HOURS)

IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID , STAR ANGLE DIFF

SLEEP PERIOD (7 HOURS)

TORQUE ANGLES: X

135:45

REESTABLISH PTC P 029 Y 315

P

Y

ROLL 0.1'/SEC 136:00 MISSION

AS503/103 MSC Form 1910 (Nov 68)

0

EDITION

FINAL

DATE

November 22, 1968

TIME

135:00 - 136:00

DAY/REV

PAGE

6/TEC

2-107

FLIGHT PLANNING BRANCH

•

0 FLIGHT PLAN

136:30

LMP

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD

MCC—H

-

M 137:00 —

137:30

CMP

CDR s.

136:00 —

S F

(7 HOURS)

-

•

138:00 — MISSION

EDITION

AS503/103

FINAL

MSC Finn 1910 (Nov 68)

TIME

DATE

November 22 o

1968 136:00 - 138:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

6/TEC

2-108

FLIGHT PLAN CMP

CDR

LMP

MCC—H 6

138:00

138:15

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

138:30

138:45

139:00 MISSION

AS503/103 MSC Form 1910 (Nov 66)

EDITION

FINAL

TIME

DATE

November 22,

196E

138:00 - 139:00

DAY/REV

6/TEC

PAGE

2-109

FLIGHT PLANNING BRANCH

0 0

•

•

FLIGHT PLAN CDR

139:00

CMP

LMP

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

MCC—H 6

LIOH CANISTER CHANGE (CARTRIDGE NO. 15 FROM A2 INTO CANISTER A)

139:15 MNVR TO P52 ATT IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF 139:30

TORQUE ANGLES: X

REESTABLISH PTC P 029 Y 315 Y P ROLL 0.1°/SEC

139:45

•

140:00 MISSION

AS503/103 MSC Form :9i

(Nay 68)

EDITION

FINAL

TIME

DATE

November 22, 196S

139:00 - 140:00

FLIGHT PLANNING BRANCH

DAY/REV

6/TEC

PAGE

2-110

FLIGHT PLAN CDR

MCC— H

CMP

OAP

SLEEP PERIOD (7 HOURS)

SLEEP PERIOD (7 HOURS)

140:0

140:15

EAT PERIOD 140:30

140:45

141 :00 MISSION

EDITION

DAT E

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

0 •

TIME

DAY/REV

-

PAGE

140:00 - 141;00

2-111

FLIGHT PLANNING BRANCH

0

j

ip

0

0 • FLIGHT PLAN MNVR TO SIGHTING ATT

LOSS OF COMM CONTINGENCY

BIOMED Sw - RIGHT'

TRN BIAS [CISLUNAR NAVIGATION P23 1. 141:15 2,

MCC—H

LMP

CMP I

CDR

141:00

STAR 22 EFH STAR E 1 SET

H

STAR 26 ENH STAR E 1 SET—

H

STAR 31 ENH STAR E H 1 SET — 141:30

EAT PERIOD -

I

EAT PERIOD

TIME

DAY/REV

141;45

142:00 MISSION

EDITION

DATE

AS503/103

FINAL

November 22,1968

MSC Form 1910 (Nov 68)

141:00 - 142:00

FLIGHT PLANNING BRANCH

PAGE

2-112

FLIGHT PL AN CMP

LMP

EAT PERIOD

EAT PERIOD

CDR

MCC-H 4

142:00

142:15

142:3

LOSS OF COMM CONTINGENCY TRN BIAS

ISLUNAR NAVIGATION P231 1.

STAR 22 EFH STAR E H 1 SET

2.

STAR 26 ENH STAR E--H 1 SET

142:45

I MISSION

AS503/103 MSC Form 1910 (Nov 68)

•

•

•

143:00 -1

0

EDITION

FINAL

TIME

DATE

November 22,1968

142:00 - 143:00

FLIGHT PLANNING BRANCH

DAY/REV

PAGE

2-113

•

0

FLIGHT PL AN CAW •

CDR

143:00

MCC- Ii

OAP

ar

P27 UPDATE: STATE VECTOR (LM & CSM SLOTS) REFSMMAT

El-3.5 HRS RECORD MNVR AND ENTRY PAD

VOICE UPDATE: MNVR PAD ENTRY PAD

143:30 MNVR TO P52 ATT IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE RI F F -- —

ECS CK

TORQUE ANGLES7— -X

EI-3 HRS

EPS CK SPS CK SM/CM RCS CK C&W CK

CMC SELF CK DSKY COND LT TEST

•

144:00 MISSION AS503/103 MSC Form 1910 (Nov 68)

EDITION FINAL

TIME

DATE November 22, 1968

143:00 - 144:00

FLIGHT PLANNING BRANCH

DAY/REV 6/TEC

2 PAGE -114

■

BURN STATUS. REPORT X - -.. X ATIG 1 X X• T

MCC'S

+ •

_

X X X

, • I W___1174 IR

XX

IP

XX

X

gx

BURN CHART P or Y RATES MCC(ALL) 10°/SEC TAKEOVER

ATT DEVIATION

SHUTDOWN TIME

10° TAKEOVER

BIT +1 SEC

RESIDUALS TRIM TO 0.2 fps

1Y !V gx iV gy

F-1

IVgz

AV C

XX

X X ; X X

X,

i

;FUEL

OX ;UNBALANCE

'REMARKS:

0 0

.

ill I

0

410

+

FLIGHT PLAN MCC-H

LMP

CMP •

CDR

144:00

EXT AV P30

EI-2.5 HRS

144:30 SPS/RCS THRUST P40/41 MNVR TO BURN ATT COAS & SXT STAR CK

GDC ALIGN TO IMU MCC 7 AV=NOMINALLY ZERO

EI-2 HRS

MCC BURN STATUS REPORT

V66 TRANS CSM STATE VECTOR TO LM SLOT

•

.145:00

MISSION

EDITION

AS503 103

FINAL

MSC Form 1910 (Nov 08)

allIMIE31.11.

DATE November 22,

196

144:00 - 145:00

FLIGHT PLANNING BRANCH

DAY/REV 7/TEC

=MI 2-115

FLIGHT PLAN CDR

LMP

CMP

MCC-H

145: 00 —

MNVR TO ENTRY ATT CCU STAR CK

LOSS OF COMM CONTINGENCY CISLUNAR NAVIGATION P23 1. STAR 33 ENH STARE H 1 SET -- --

BIOMED Sw - LEFT

SXT STAR CK IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , -STAR ANGLE DIFF

EI-1.5 HR

PIPA BIAS CK

TORQUE ANGLES: X Y

145:30 — GDC ALIGN TO IMU FINAL STOWAGE

E I -1 HR

FINAL STOWAGE INITIATE CM RCS PREHEAT WASTE H 2 O DUMP - OFF UR DUMP HT - OFF

FINAL STOWAGE

EMS CK

FINAL GDC DRIFT CK 146:00 —1 MISSION

AS503/103_ MSC form 1310 (Nov 68)

•

0

EDITION

FINAL

TIME

DATE

November 22, 196E

145:00 - 146:00

FLIGHT PLANNING BRANCH

r

DAY/REV

7/TEC

•

PAGE

2-116

4I■

0 FLIGHT PL AN MCC—H

LMP

CMP

CDR

I

•

146:00

TERM CM RCS PREHEAT SET DET TO EI EMS INITIALIZATION RSI ALIGN TO GDC CM RCS CK

PYRO BAT CK

RECORD ENTRY PAD & RCVY INFO

P27 UPDATE: STATE VECTOR VOICE UPDATE: ENTRY PAD & RCVY INFO

ENTRY BATS - ON

EI-30 MIN

146:30 EI-15 MIN

SEPARATION CK LIST

SEPARATION CK LIST

SEPARATION CK LIST

MNVR TO CM/SM SEP ATT

P61 ENTRY PREP

GO FOR PYRO ARM

GO FOR PYRO ARM

[CM/SM SEP MNVR TO ENTRY ATT

P62 ENTRY ATTITUDE

P63 ENTRY INITIATE [ET = 4QOK1

146:50

P64 ENTRY POST .05G

147:00 MISSION

EDITION

DATE

TIME

AS503/103

FINAL

November 22, 1968

146:00 - 147:00

MSC Form 1910 (Nov 98)

FLIGHT PLANNING BRANCH

DAY/REV

7/TEC

PAGE

2-117

FLIGHT PLAN 147 : 00 —

CMP

CDR •

•

LMP

•

MCC-H •

EARTH LANDING PHASE

LSPLASHDOWN

147:30 —

•

148:00 — MISSION

SE03/103 MSC Form 1910 (Nov 60)

0 0

EDITION

FINAL

DATE

November 22, 1968

TIME

147:00 - 148:00

DAY/REV

PAGE

2-118

7/TEC

FLIGHT PLANNING BRANCH

•

•