01 1,1 4. 'T if, 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

Approved by: et,

,,, W. J. North Chief, Flight Crew Support Division

, Dona d'IC. Slayton Director of Flight Cre4 Operations

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

Concurrence: / 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 3-45 Section IV - Detailed Test Objectives 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 Opera- tional 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

Accelerometer Constant Delta Altitude ACCEL ODE Activation Commander ACT CDR ACQ Acquisition CDU Control Data Unit Abort Electronics Assembly Circularization AEA CIRC Abort Guidance Sybsystem Check AGS CK Command Module . Ali Ampere Hours CM ALIGN Alignment CMC Command Module Computer ALT Altitude CONT Continue AMP or amp Ampere CMD Command AMPL Amplifier CMP Command Module Pilot ANG Antigua CNTL Control Ant Antenna CNTLS Controls AOS Acquisition of Signal C.O. Cut off AOT Alignment Optical Telescope Check out C/O Ascent Propulsion Subsystem Crew Optical Alignment Sight APS COAS Atmosphere Revitalization Communications ARS COMM H. Computational ASC Ascension COMP Ascent CONFIG Configuration AS CT Attitude CP Control Point ATT AUX Auxiliary CR0 Carnarvon, Australia AZ Azimuth CRY 0 Cryogenic CSI Coelliptic Sequence Initiation Maneuver BAT Battery CSM Command Service Module BDA Bermuda C&WS Caution and Warning System BP Barber Pole GYI Grand Canary Island BT Burn time Bio Bio-Medical Data on Voice Downlink DAP Digital Auto Pilot B iW Black & white D/B Deadband BU Backup DEDA Data Entry and Display Assembly BRKT Bracket DEGS Degrees Depletion DEPL CAL Pt. Arquillo, California Determination or Digital Event Timer DET CAL Difference Calibration Angle DIFF CAM Docked Camera DK CB Circuit Breaker DOI Descent Orbit Insertion ABBREVIATIONS (Cont'd)

DP S Descent Propulsion Subsystem GET Ground Elapsed Time DSE Data Storage Equipment GETI Ground Elapsed Time of Ignition DSKY Display and Key Board GLY Glycol DIO Detailed Test Objective GMT Greenwich Mean Time DUA Digital Uplink Assembly G&N Guidance and Navigation DWN Down GNCS Guidance Navigation Control System GWM Guam E Erasable GYM Guaymas, Mexico ECS Environmental Control Subsystem EPH Earth Far Horizon HA Apogee Altitude EI Earth (atmosphere) Interface HAW Hawaii ELDMK Earth Landmark HBR High Bit Rate (TLM) EMS Entry Monitor System HD Highly Desirable ENU Earth Near Horizon HGA High Gain Antenna EPO Earth Parking Orbit HI High EPS Electrical Power Subsystem Hp Perigee Altitude EQUIP Equipment HSK Honeysuckle (Canberra, Australia) EST Eastern Standard Time HTR Heater EVAP Evaporator HTV USNS Huntsville EVT Extravehicular Transfer EXT External ID Identification IGN Ignition F Stop IAN Inertial Measurement Unit FC Fuel Cell INIT Initialization FDAI Flight Director Attitude Indicator INT Intervalometer FLT Flight IP Initial Point FM Frequency Modulated IU Instrumentation Unit FOV Field of View I VT Intravehicular Transfer fps Feet per second FQ Flight Qualification JETT Jettison FT or ft Feet FTP Full Throttle Position kwh Kilowatt Hour

GBI Grand Bahama LAT Latitude GDC Gyro Display Coupler LBR Low Bit Rate (TLM) GDS Goldstone, California LBS or lbs Pounds 0 0 •

ABBREVIATIONS (Cont'd)

LCG Liquid Cooled Garment MEAS Measurement LDG Landing MER DSNS Mercury LDMK Landmark MET Mission Event Timer LEB Lower Equipment Bay M/I Minimum Impulse LFH Lunar Far Horizon MIN Minimum LGC LM Guidance Computer. MLA Merritt Island LH Left-hand MNVR Maneuver L/H Local Horizontal MON Monitor LHEB Left-hand Equipment Bay MSFN Manned Space Flight Network LHFEB Left-hand Forward Equipment Bay MTVC Manual Thrust Vector Control LION Lithium Hydroxide LLM Lunar Landing Mission NAV Navigation LLOS Landmark Line of Sight NCC Corrective Combination Maneuver LM Lunar Module TIM Nautical Miles LMP Lunar Module Pilot NOM Nominal LNH Lunar Near Horizon NSR Nominal Slow Rate LOT Lunar Orbit Insertion NXX Noun XX LONG Longitude LOS Loss of Signal OBS Observation LPO Lunar Parking Orbit 0/F Oxidizer to Fuel LR Landing Radar OP ER Operate LT Light ORB Orbital LTG Lighting ORDEAL Orbit Rate Display Earth and Lunar LV Launch Vehicle ORIENT Orientation L/V Local Vertical OVHD Overhead LVPD . Launch Vehicle Pressure Display P Pitch M Mandatory PAD Voice Update MAD Madrid, Spain PCM Pulse Code Modulation MAN Manual PC Pericyntiian MAX Maximum PGA Pressure Garment Assembly MAX Q Maximum Dynamic Pressure PCNCS Primary Guidance Navigation Control Section MCC Midcourse Correction PIPA Pulse Integrating Pendulous Accelerometer MCC-N Mission Control Center,- Houston PM Phase Modulated MDC Main Display Console P OL Polarity or Polarizing ABBREVIATIONS (Cont'd)

PREF Preferred S Shaft PREP Preparation SA Shaft Angle PRESS Pressure S/C Spacecraft PRIM Primary SCE Signal Conditioning Equipment PT Point SCS Stabilization Control System PRN Pseudo-Random Noise SCT Scanning Telescope PROP Proportional SEC Secondary PU Propellant Utilization SECO S-IVB Engine Cut-off PUGS Propellant Utilization and Gaging System SEP Separate PTC Passive Thermal Control SEQ Sequence PWR Power SLA Service Module LM Adapter Pxx Program XX SLOS Star Line-of-Sight SM Service Module Qty Quantity SPOT Spot Meter SPS Service Propulsion System R Roll SR Sunrise R&B Red & Blue SRX S-Band Receiver Mode No. X RAD Radiator SS Sunset RCDR Recorder STX S--Band Transmit Mode No. X RCS Reaction Control Subsystem STBY Standby RCU Remote Control Unit Sw Switch RCV Receiver SXT Sextant RED USNS Redstone SYNC Synchronization REFSMMAT Reference Stable Member Matrix REG Regulator T Trunnion REQD Required T Time of Ephemeris Update RH Right-hand EPHEM RNDZ Rendezvous TA Trunnion Angle RR Rendezvous Radar TAN Tananarive RSI Roll Stability Indicator TCA Time of Closest Approach RT Real Time TBD To Be Determined RTC Real-Time Command TEC Trans Earth Coast Rxx Routine XX TEI Transearth Insertion

0 0 ABBREVIATIONS (Cont' d)

Velocity Change (Differential) TEMP Temperature AV Terminate Velocity Change at Engine Cutoff TERM AV C TEX Corpus Christi, Texas AR Position Change (Differential) T &D Transposition and Docking TGT Target 8-balls Flight Director Attitude Indicator (FDAI) TIC Time of Ignition LBS or lbs Pounds TLC Trans Lunar Coast TLI Translunar Insertion TLM Telemetry CAMERA NOMENCLATURE TPF TeLwinal Phase Final TPI Terminal Phase Initiation 2/80/B3 - Hasselblad No. 2/80mm Lens/Stowage Location TPM Terminal Phase Midcourse 16/18/20 - 16mm Camera/18mm Lens/20 Frames Per Second T/R Transmitter/Receiver 1/150/New B&W/INT - Hasselblad No. 1/150mm Lens/VSE New TRANS Translation B&W Magazine/with interferometer TV Television C-EX - color film - external

TVC Thrust Vector Control POL FILTER 1/4 - Polarization filter, Shutter Speed 1/4 TWR Tower S0368 - Type of External Film 2/80/H.S. - Hasselblad No. 2/80mm Lens/High Speed Film UMB Umbilical Cable/BRRT/R&B - Use Power Cable, Camera Mounted on Bracket UNDK Undock with Red & Blue Filter US United States Pass

VHF Very High Frequency VLV Valve Vxx Verb xx

W / 0 Without WRT With Respect to WTN USNS Watertown

XFER Transfer XMIT Transmit or Transmitter XPONDER Transponder

Yaw 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 con- strained 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 trans- • earth 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.

After 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. 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 410 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 LOI1 .

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 prep- aration, 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 LOI2 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 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 Prime Backup Commander (CDR) Left Borman Armstrong Command Module Pilot (CMS) Center Lovell Aldrin Lunar Module Pilot (LMP) Right 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. Lift-off -45 seconds through 0:12:00 GET b. TLI -2 minutes through TLI cutoff +1 minute c. CSM/S-IVB Sep -2 minutes through Sep +1 minute d. 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 02 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.

IMU drift checks are scheduled. after TLI, before on 4. LOIl' 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

ALTITUDE CSM SIGNAL GROUND GET nm ANTENNA COMBINATION ANT COMMUNICATIONS MODE

03:20 OMNI 4.2 85' GDS Carrier,PRN,voice, 51.2 KBPS TM

05:45 24,000 HI GAIN 4. 2 85' GDS Carrier,PRN,voice, HBR TM 24,000 HI GAIN 6.2 85' GDS Oarrier,PRN,Voice, HBR TM 24,000 HI GAIN .2 85' GDS Plybk of Recorded Voice & LBR TM

07:00 35,000 HI GAIN 4.3 85' GDS Carrier,PRN,voice, LBR TM to 35,000 HI GAIN 6.3 85' GDS Carrier,PRN,voice, LBR TM 08:00 35,000 HI GAIN 5.2 85' GDS Carrier,PRN,voice HBR TM 35,000 HI GAIN 8.1 85' GDS Carrier,voice and LBR TM

29:00 110,000 HI GAIN 4 30' ASC Carrier, PRN, Voice to 110,000 HI GAIN 5 30' ASC Carrier, PRN, Updata 30,000 110,000 HI GAIN 6 30' ASC Carrier, PRN, Voice, Updata or 110,000 HI GAIN 8 30' ASC Carrier, BU Voice 125,000 110,000 HI GAIN 4.2 30' ASO Carrier, PRN, Voice, HER TM to 110,000 HI GAIN 5.2 30' ASC Carrier, PRN, Voice, HBR TM 126,000 110,000 HI GAIN 4.3 30' ASC Carrier, PRN, Voice, LBR TM 110,000 HI GAIN 8.1 30' ASC Carrier, Voice, HBR TM 110,000 OMNI 1 30' ASO Carrier, PRN 110,000 OMNI .5 30' ASC Carrier, LBR TM 110,000 OMNI .6 30' ASC Carrier, Key Subcarrier 110,000 OMNI 1.7 30' ASC Carrier, PRN Ranging 110,000 OMNI .8 30' ASC Carrier, BU Voice, LBR TM 110,000 OMNI .10 30' ASC Carrier, BU Voice

31:15 120,000 HI GAIN .4 85' GDS CSM Television NORMAL OPERATING MODES 69:00 205,000 HI GAIN 6.2 85' Carrier, PRN, Voice, HBR TM 205,000 HI GAIN 6.3 85' Carrier, PRN, Voice, LBR TM 205,000 HI GAIN .2 85' Plybk of Recorded voice &LBR TM

89:00 205,000 HI GAIN .4 85' CSM television

1-6 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 ; a ' TB6p X x x x X . X H IR i X X X X X X P X X X X X X . Y X X X ; X X X ; BT • , .8VC I + + VI X X X X , X ,.X . R SEP X X X X X X - P SEP X X X X X X Y SEP TLI PAD TB6p X:XX:XX(HRS:MIN:SEC) PREDICTED TIME OF BEGINNING OF S-IVB RESTART PREPARATION FOR TLI (TB6 TLI IGN -9 MIN) R XXX (DEG) PREDICTED SPACECRAFT IMU XXX (DEG) GIMBAL ANGLES AT TLI Y XXX (DEG) 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 XXX (DEG) PREDICTED SPACECRAFT IMU P SEP XXX (DEG) GIMBAL ANGLES AT COMPLETION Y SEP XXX (DEG) OF S-IVB MNVR TO CSM/S-IVB SEP ATTITUDE P27 UPDATE PURP V V GET • • IS 304 0 INDEX INDEX INDEX 02 03 • 04 05 06 F 1-- 07 10 II 12 13 14 15 ' 1 6 17 20 2I 22 23 24

N34 HRS X X X X X X MIN X X XX X X•X X NAV CHECK SEC X X X•X • I N43 LAT 0 • 0 , LONG _• , 1 ALT + 0 + 0 '

1 - b • 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 TO CONFIRM POINT ABOVE GROUND CHECK 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 P.S'OP/GUk:) SET STARS WT ;. J 47 R ALIGN 0 0 PTRhA " 8 P ALIGN 0 0 YTRI: A Y ALIGN I+ 0 0 HRS GET + 0 0 WN N33 + 0 SEC nvx NE-1 ULAGE U • LIVy

• nVZ X X X R X X X HX X X N4-3- 1

P •

• :]VT HORIZON/WINDOW X X X • i3T X .]VC X XX X SXTS 0 SFT • . 0 SRN X X X BSS SPA X X • , X X XI S X P OTH ER 0 LAT N61 LONG 11/_----,L-- RTGO EMS VIO • • I GET .05G • •

1-12 MANEUVER PAD PURPOSE XXXXXX TYPE OF MNVR TO BE PERFORMED PROP/GUID 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 TIME OF MNVR IGNITION (HRS:MIN:SEC) AVX XXXX.X (fps) P30 VELOCITY TO BE GAINED AVY XXXX.X (fps) COMPONENTS IN LOCAL VERTICAL AVZ XXXX.X (fps) COORDINATES R XXX (DEG) IMU GIMBAL ANGLES OF P XXX (DEG) MANEUVER ATTITUDE Y XXX (DEG) H XXXX.X (nm) PREDICTED APOGEE ALTITUDE A AFTER MANEUVER H XXXX.X (nm) PREDICTED PERIGEE ALTITUDE P AFTER MANEUVER AVT 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 1-13 MANEUVER PAD (cont'd) SXP X.X (DEG) BSS X POSITION ON COAS LAT XX.XX LATITUDE AND LONGITUDE OF THE LONG XXX.XX 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 & STARS FOR TELESCOPE FOR SOUTH BACKUP GDC ALIGN SET STARS R, P, Y ATTITUDE TO BE SET IN

( ALIGN) ATTITUDE SET TW FOR BACKUP GDC ALIGN ULLAGE NO. OF SM RCS JETS USED AND LENGTH OF TIME OF ULLAGE HORIZON WINDOW MARKING AT WHICH WINDOW HORIZON IS PLACED AT A SPECIFIED TIG (ATT CK) ENTRY AREA xIxIx X X R .05G x xxix X X X P .05G X X X Y .05G GET HOR • X X X P CK 0 LAT N6 I LONG X X MAX G

V400K N60 0 0 , 0 0 T4OOK + RTGO EMS + 4- 1 VIO • • • RRT x x • X X • RET. 05G * + 0 0 + 0 ' 0 DL MAX - *N69 + 0 0 . +i 0 0 • DL M IN • VL MAX* * I VL M I N

X X X X . X X Do • X X • X X • RET VCIRC • • X X • X 4 X . • RETB BO • x x: X , X • RETEBO • X X • X X • RETDRO X :X . X X X X X X SX TS SFT !O 0 ;0 0 TRN X X X X X X BSS X X X X • _ SPA X X X X X X • SXP X X X X. X X X X LIFT VECTOR

1-15 ENTRY PAD AREA XXX SPLASHDOWN AREA DEFINED BY TARGET LINE R .05G XXX(DEG) SPACECRAFT IMU GIMBAL ANGLES P .05G XXX(DEG) REQUIRED FOR AERODYNAMIC Y .050 XXX(DEG) TRIM AT .050 GET XX:XX:XX TIME OF ENTRY ATTITUDE (H0R CK) (HRS:MIN:SEC). HORIZ CHECK AT EI -17 MIN. P XXX(DEG) PITCH ATTITUDE FOR HORIZON (HOR CK) 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

400K XXXXX (fps) INERTIAL VELOCITY AT ENTRY V 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 TIME OF .05G FROM 400K (RRT) (MIN:SEC) D L MAX X.XX (G's) MAXIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC) D MIN X.XX (G's) 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 XX:XX TIME FROM EI THAT S/C VELOCITY CIRC (MIN:SEC) BECOMES CIRCULAR

RETBBO XX:XX TIME FROM EI TO THE BEGINNING (MIN:SEC) OF BLACKOUT

RETEBO XX:XX TIME FROM EI TO THE END OF (MIN:SEC) BLACKOUT RETDRO XX:XX TIME FROM ET TO DROGUE DEPLOY (MIN:SEC) 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 REMARKS GET (hrs:min:sec) LOS 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 REMARKS GET (hrs:min:sec) LOS

PM .• .•

• AOS .- -. SS .

REV 8/9 REMARKS GET (hrs:min:sec)

LOS .

SR .• •.

PM ' : AOS :

SS .- -.

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

REV 10 REMARKS GET (hrs:min:sec)

LOS - SR .•

ADS .• • SS '

1-19 MAP UPDATE

REV 4/5 REMARKS 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 REMARKS GET (hrs:min:sec) *

LOS .

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 ACQUISITION OF SIGNAL

SS XX:XX:XX(HRS:MIN:SEC) TIME OF SPACECRAFT SUNSET IN • LUNAR ORBIT 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)

•

1-21 •_:.. •

SECTION II - DETAIL-RD TTNELIn e

• e •

• 0 0 0

FLIGHT PLAN , TIME EVENT REMARKS -00:45 LMP: FLT RCDR - RECORD -00:09 LCC: IGNITION COMMAND -00:01 L/V ENGINE LTS (5) - OUT 00:00 LCC:CDR: REPORT LIFT-OFF LIFT-OFF LT - ON, MET STARTS COUNT P11 AUTO

00:02 CDR: REPORT YAW MNVR , 00:11 CDR: REPORT ROLL AND PITCH PROGRAM INITIATE 00:28 CDR REPORT ROLL COMPLETE .00:42 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

MISSON AS503/103 EDITION FINAL DATE November 22,1968 PAGE 2-1

MSC FORM 2114C (JUL 67) FLIGHT PLAN

TIME EVENT REMARKS

03:00 CDR: REPORT 2ND PLANE SEP >65% THRUST-S-II SEP LIGHT OUT 03:07 CDR: REPORT TWR JETT & MODE II 03:25 CDR: REPORT GUIDANCE INITIATE 03:53 MCC-H: REPORT TRAJECTORY AND GUID. 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 IF LAUNCH AZIMUTH <90 0 07:00 CDR: REPORT S/C GO/NO GO 08:00 08:20 MCC-H:CDR: REPORT GO/NO GO FOR STAGING 08:40 CDR: REPORT S-II CUTOFF, S-II STAGING

MISSON A5503/103 EDITION FINAL DATE November 22,1968 PAGE 2-11

MSC FORM 2114C {SUL 67)

0 • 0 0 FLIGHT PLAN

TIME EVENT REMARKS 08:45 CDR: REPORT S-IVB IGNITION 09:00 CDR: REPORT S/C GO/NO GC MCC-H: REPORT TRAJECTORY AND GUID. - GO/NO GO

09:50 MCC-H:CDR: REPORT MARK MODE IV 10:00 MCC-H:0DR: REPORT GO/NO GO FOR ORBIT MCC-H: REPORT PREDICTED TIME OF SECO 11:21 CDR: REPORT SECO AND HP 11:31 MCC-H:CDR: REPORT ORBITAL GO/NO GO 12:00 LMP: FLT RCDR - OFF

MISSON AS503/103 EDITION FINAL DATE November 22, 1968 PAGE 2-iii

MSC FORM 21140 (JUL 67) FLIGHT PLAN

CDR CMP LMP MCC-H 00:00 • •

POST INSERTION CONFIG POST INSERTION CONFIG POST INSERTION CONFIG SM RCS CK CM RCS CK 00:15 REMOVE HELMET & GLOVES C&W CK REMOVE HELMET & GLOVES REMOVE HELMET & GLOVES ECS POST INSERTION ECS POST INSERTION CONFIG CONFIG CDC ALIGN TO IMU INGRESS LEB EPS PERIODIC MONITOR T 0 MAIN'REG CK C 2 ECS MONITOR CK 00:30 MOUNT & INITIALIZE SPS PERIODIC MONITOR ORDEAL PUGS TEST INSTALL COAS JETTISON OPTICS COVER ECS REDUNDANT COMP CK T A COAS HORIZON CK RECORD AAZ CORRECTION FC PURGE OK VOICE N UPDATE: AAZ CORREC- TION 00:45

1- OPTICS CK IMU REALIGN P52 ] RC OPTION 3 - REFSMMAT BIOMED Sw - CENTER 0 STAR ID J- —Tc'Erit'd) 01:00 •

MISSION EDITION DATE TIME DAY/REV PAGE 2-1 AS503/103 FINAL November 22,1968 00:00 - 01:00 1 /LPO MSC Form 1910 (0T) Oct 68) FLIGHT PLANNING BRANCH 0 0 0 0 • • 0 41 FLIGHT PLAN CDR CMP LMP 01:00 • • STAR ANGLE RIFF S TORQUE ANGLES:. X __. Y

01:15

REPORT: GYRO TORQUE 01:30 ANGLES BACKUP COMM CK GIVE GO FOR SCS ATT REFERENCE COMM CK COMPARISON CK RECORD ABORT BLOCK PAD VOICE UPDATE: (TLI +90 MIN AND TLI BLOCK +4 HOUR) DATA

01:45 RECORD TLI PAD VOICE UPDATE: TLI PAD P27 UPDATE: Y BIOMED Sw - RIGHT STATE VECTORS

02:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 01:00 - 02:00 1/LPO 2-2 MSC Form 1510 (OT) ( Oct 68) FLIGHT PLANNING BRANCH

BURN STATUS REPORT TLI X X ATIG BURN CHART X X BT P or Y ATT SHUTDOWN V gx RATES DEVIATION TIME RESIDUALS TRIM 10°/SEC TLI +45° B/T+6 SEC & X X X R SHUTDOWN SHUTDOWN Vi=PAD VALVE NO TRIM X X X P X X X Y TLI PREMATURE SHUTDOWN Vi ha >60,000 nm LUNAR ORBIT OR FLYBY (DEPENDING ON AV REQD: ha >22,000 nm TWO PHASING MANEUVERS TO SEMI-SYNCHRONOUS ORBIT. DIRECT ENTRY h ha >41,000 nm HIGH ALTITUDE ORBITS FOLLOWED BY DEBOOST AV TO 400 nm APOGEE c X X X FUEL h a 100 - 41,000 nm EITHER HI ALTITUDE (41,000 ha) OR LOW ALT, DEPENDING ON LANDMARKS X X X Ox I XXX UNBALANCE REMARKS:

0 0 0 • 0 • FLIGHT PLAN

CDR CMP LMP MCC-H • • •

TLI PREP TLI PREP TLI PREP EMS AV TEST TRANS TO COUCH

GO/NO-GO FOR PYRO ARM GO/NO-GO GO/NO-GO FOR TLI

GDC ALIGN AND DRIFT CK BIOMED Sw - LEFT

TB-6

P47 BURN ATT CK FLT RCDR - RECORD IGETI = 2:50:31

SECO S-IVB INERTIAL FLT RCDR - OFF SECO +20 SEC S-IVB TO LH 2 ORB RATE,HEADS DOWN •

MISSION EDITION DATE TIME DAY/REV MOE 1/LPO 2-3 AS503/103 FINAL November 22,1968 02:00 - 03:00 MSC Form 1910 (0T) (Oct 68) FLIGHT PLANNING BRANCH

FLIGHT PLAN

CDR CMP LMP MCC-H 03:00 • RECORD GET SEP MNVR VOICE TLI BURN STATUS REPORT INIT UPDATE: GET OF SEP TRANS CSM STATE VECTOR MNVR INIT S-IVB MNVR TO SEP ATT TO LM SLOT UNSTOW PHOTO EQUIP B3 16mm DAC 03:15 GO/NO-GO FOR 90-MIN 18mm LENS GO/NO-GO ABORT RT ANG MIRROR 16mm C-EX MAG S-BAND XPONDER - SEC COMM TEST PWR CABLE TRANSPOSITION FROM 70mm CAM FLT RCDR - RECORD MODE: 4.2 S-IVB +X FOR 1 fps, 80mm LENS COAST FOR 1 MIN, -X 70mm C-MAG FOR 0.5 fps, PITCH UP FLT RCDR - OFF 4°/SEC R13 SPOTMETER NONESS BUS - OFF 03:30 PHOTOGRAPH S-IVB FLY FORMATION DOFF & STOW PGA 16/18/C-EX, 1/250, fll, 6 fps (1 MAG) 2/80/C, 1/250, SPOT (10 EXP)

03:45 MNVR TO LOCAL VERTICAL -X RADIALLY UPWARD 1,5 fps

TRANS CSM STATE VECTOR TO LM SLOT 04:J a •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 03:00 - 04:00 1/TLC 2-4 MSC Form 1910 (0T) (Oct 68) FLIGHT PLANNING BRANCH • 0 0 0 • • • FLIGHT PLAN

CDR CMP LMP MCC—H • 04:00 fi IMU REALIGN P52 REPORT PERSONAL OPTION 3 - REFSMMAT RADIATION DOSIMETER STAR ID READINGS STAR ANGLE DIFF TORQUE ANGLES: X Y 04:15 _

GDC ALIGN TO IMU r CISLUNAR NAVIGATION P231 TRN BIAS 1. STAR 14 ENH STAR E H 1 SET - 3 MARKS EACH

2. STAR 15 EFH STARE H 2 SETS - 3 MARKS EACH

04:45 —

3. STAR 16 EFH STAR E H 2 SETS - 3 MARKS 05:00 -- EACH •

MISSION EDITION DATE TIME DAY/ REV PAGE AS503/103 FINAL November 22,1968 04:00 - 05:00 1/TLC 2-5 MSC Form 1910 (Nov 68) FLIGHT PLANNING IRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 05 :00 — • 6 RECORD BLOCK DATA VOICE GROUND TRACK DET P21 (TLI +4 HRS & UPDATE: TLI +11 HRS) BLOCK DATA DOFF & STOW PGA

05:15 - BIOMED Sw - CENTER

MNVR TO PTC ATT P 331 Y 331 P Y roll 0.1°/SEC DOFF & STOW PGA 05 :30 — F

COMM TEST MODES: KEY V64 S-BAND HIGH GAIN ANT 4.2 CHECKOUT 05:45 - 6.2 .2 FM DSE DUMP

06:00 • a

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 05:00 - 06:00 1/TLC 2-6 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0 • 0 411) • • FLIGHT PLAN

CDR CMP LMP MCC-H 06:00

06:15

06:30 EAT R RIOD EAT PERIOD EAT PERIOD

06:45

07:00

MISSION EDITION DATE - TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 06:00 - 07:00 1/TLC 2-7 MSC Form 1 FLIGHT PLANNING BRANCH

FLIGHT PLAN LMP MCC—H CDR• CMP 07:00 PERFORM COMM TESTS MODES: 4.3 6.3 5.2 8.1

07:15 —

LiOH CANISTER CHANGE (CARTRIDGE NO. 3 FROM 07:30 A3 INTO CANISTER A)

OPEN COOLANT CONTROL ATTENUATION PANEL EVAP WATER CONT SEC VLV - OFF

07:45 — CLOSE COOLANT CONTROL ATTENUATION PANEL

I WASTE STOWAGE VENT - CLOSED P27 UPDATE: BAT VENT VLV - OPEN STATE (UNTIL SERVICE VECTOR METER = 0) TGT LOAD 08:00 BAT VENT VLV - CLOSED •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 07:00 - 08:00 1/TLC 2-8 MSC Form 191U (Nov 08) FLIGHT PLANNING BRANCH

0 0 0 0

MCC'S BURN STATUS REPORT X x 1 1 • ; ATIG BURN CHART X x • ST V P or Y ATT SHUTDOWN gx RATES DEVIATION TIME RESIDUALS .TRIM X X X R MCC(ALL) 10°/SEC 10 0 B/T +1 SEC TRIM TO 0.2 fps TAKEOVER TAKEOVER X X X P X X X Y .V gx V • _ gY V gz Co AV c X X X FUEL X X X Ox X X X UNBALANCE 'REMARKS: FLIGHT PLAN

CDR CMP LMP MCC—H 08:00 • • • MNVR TO P52 ATT IMU REALIGN P52 VOICE OPTION 3 - REFSMMAT UPDATE: AND DRIFT CK MNVR PAD STAR ID RECORD MNVR PAD STAR ANGLE DIFF

TORQUE ANGLES -- -- X 08:15 Y

V47 TRANS LM STATE VECTOR TO CSM SLOT BIOMED Sw - RIGHT 08:30 EXT AV P30 PIPA BIAS SPS/RCS THRUST P40/P41 CK MNVR TO BURN ATT SXT STAR CK

TRANS TO COUCH

08:45 EMS AV TEST

GDC ALIGN TLI +6 HRS 09:00 :1 MCC, AV--NOtilINALLY ZERO

PAGE MISSION EDITION DATE TIME DAY/REV AS503/103 FINAL November 22,1968 08:00 - 09:00 1/TLC 2-9 MSC Form 1910 (Nov 66) FLIGHT PLANNING ANCH 0 9 0 • FLIGHT PLAN

CDR CMP LMP MCC-14 09:00 • V66 TRANS CSM STATE SPS MONITOR CK VECTOR TO LM SLOT SM RCS CK INITIATE BAT CHARGE MCC 1 BURN STATUS REPORT TRN BIAS MNVR TO SIGHTING ATT CISLUNAR NAVIGATION P23 STAR 15 ELDMK 10 LAT 28.876 ° N LONG/2 56.292 ° W ALT 000.01 STAR ELDMK LAT -- LONG/2 ALT 2 SETS 09:30

. STAR 16 ELDMK 10 LAT 28.876°N LONG/2 56.292 ° W ALT 000.01 STAR ELDMK LAT LONG/2 MNVR TO PTC ATT ALT P 331 Y 331 GROUND TRACK DET P21 P Y ROLL 0.1 ° /SEC

10 :0 0

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 09:00 - 10:00 1/TLC 2-10 MSC Form 1910 (Nov 88) FLIGHT N FLIGHT PLAN CDR CMP LMP MCC— H 10:00 • • • •

10:30 — EAT PERIOD

S 11:00 F

11:30 SLEEP PERIOD BIOMED Sw - CENTER (7 HOURS)

12:00

MISSION EDITION DATE TIME DAY/REV PAGE

AS503/103 FINAL November 22,1968 10:00 - 12:00 1/TLC 2-11 . WSC Form i910 (Nov 51) FLIGHT PLANNING BRANCH

0 0 ft' 0 • 0 • FLIGHT PL AN

CDR CMP LMP MCC-H 12:00 • RECORD BLOCK DATA VOICE

(TLI +11 HOURS, TLI +25 . UPDATE: HOURS, & FLY BY) BLOCK DATA

12:30

M SLEEP PERIOD 13:00 S (7 HOURS) F N

13:30

14:00, •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 12:00 - 14:00 1/TLC 2-12 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC— H • 14:00 •

14:30 BIOMED Sw - RIGHT

1 S SLEEP PERIOD 15:00 F (7 HOURS

15:30 EAT PERIOD I EAT PERIOD

16:00

MISSION EDITION DATE TIME DAY" REV PAGE 2-13 AS503/103 FINAL November 22,1968 14:00 - 16:00 1 /TLC MSC Form 1910 (Nov 69) FLIGHT PLANNING BRANCH

0 0 ra • • • • FLIGHT PLAN

CDR CMP LMP MCC—H 16:00 •

16:15

M SLEEP PERIOD 16:30 S (7 HOURS) MNVR TO P52 ATT F N

IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF 16:45 TORQUE ANGLE: X Y

CDC ALIGN TO IMU MNVR TO SIGHTING ATT SCT STAR VISIBILITY

17:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103. FINAL November 22,1968 16:00 - 17:00 1/TLC 2-14 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 17:00

TRN BIAS 17:15

CISLUNAR NAVIGATION P23I 1. STAR 22 EFH STAR E H 3 SETS

17:30 SLEEP PERIOD (7 HOURS) 2. STAR 16 EFH STAR E H 2 SETS --

17:45 GROUND TRACK DET P21

BIOMED Sw - LEFT 18:00—

MISSION EDITION DATE TIME T DAY/REV. PAGE AS503/103 FINAL November 22,1968 17:00 - 18:00 1/TLC 2-15 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0 0 0 • FLIGHT PLAN CDR CMP MCC-I4 18:00 MNVR TO PTC ATT LiON CANISTER CHANGE P 331 Y 331 (CARTRIDGE NO. 4 FROM P Y A3 INTO CANISTER B) ROLL 0.1°/SEC

18:30

19:00 5 EAT PERIOD SLEEP PERIOD SLEEP PERIOD N (7 HOURS) (7 HOURS)

19:30 CDR CREW STATUS REPORT

20:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 18:00 - 20:00 1/TLC 2-16 MSC Form 1910 (Nov Be) FLIGHT I ER FLIGHT PLAN

CDR CMP LMP MCC -H 6 20:00 —

20:30 -

••

21:00 — SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

21 30— I

22: 0.0 -1

MISSION EDITION DATE TIME DAY/REV PAGE 2-17 AS503/103 FINAL November 22, 1968 20:00 - 22 :00 1/TLC MSC Form 19I0 (Nov 98) FLIGHT PLANNING BRANCH • • S 0 0 • • fi FLIGHT PL AN CDR CMP LMP MCC— H 22;00

22:30

23:00 SLEEP PERIOD SLEEP PERIOD F (7 HOURS) (7 HOURS)

23:30

24:00 1

MISSION EDITION DATE TIME DAWREV PAGE AS503/103 FINAL November 22,1968 22:00 - 24:00 1/TLC 2-18 MSC Form 1910 (Nov 60 FLIGHT PLANNING BRANCH FLIGHT PL AN CDR CMP IMP MCC-H 24:00 —

24:30 - SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

S 25:00 - F N RECORD BLOCK DATA BIOMED Sw CENTER VOICE (TLI + 25 HOURS, & UPDATE: TLI + 35 HOURS, & BLOCK DATA FLY BY )

25:30- EAT PERIOD EAT PERIOD I EAT PERIOD

MNVR TO P52 ATT 26:00—

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 24:00 - 26:00 2/TLC 2-19 MSC Form 1610 (Nov 68) FLIGHT PLANNING BRANCH 0 FLIGHT PLAN CDR• CMP LMP MCC—H 26:00 CMP/LMP CREW STATUS REPORT IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFT-- -- TORQUE ANGLES: 26:15 X

GDC ALIGN TO IMU TRN BIAS M NVR TO SIGHTING ATTITUDE

26: 30 1CISLUNAR NAVIGATION P23I . STAR 16 EFH STAR E 1 ET

. STAR 22 EFH STAR E H 26:45 1 SET

3. STAR 26 ENH STAR E H 1 SET VOICE UPDATE: RECORD MNVR PAD MNVR PAD 27:0 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 26:00 - 27:00 2/TLC 2-20 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH

BURN STATUS REPORT MCC'S ; X X : I ATIG BURN CHART — X X _ _ V P or Y ATT SHUTDOWN g x RATES DEVIATION TIME RESIDUALS

X X X MCC(ALL) 10°/SEC 10° B/T +1 SEC TRIM TO 0.2 fps — 7 TAKEOVER TAKEOVER X X X. I ID X X X y I V gx j 9Y gz . —r ;AV 1 C X X X FUEL X X X .0X X X X 1 ' UNBALANCE 'REMARKS:

0 • is 0 O 0 0 S FLIGHT PLAN IMP MCC-H CDR CMP 6 • 27:00 • GROUND TRACK DET P21 P27 UPDATE: STATE VECTOR TGT LOAD

27:15 V47 TRANS LM STATE VECTOR TO CSM SLOT EXT AV P30

27:30 SPS/RCS THRUST P40/41 PIPA BIAS MNVR TO BURN ATT CK

SXT STAR CK TRANS TO COUCH

27:45 EMS AV TEST

TLI + 25 HRS GDC ALIGN SM RCS MON CK MCC AV=NOMINALLY ZER • 28:00 2

TIME DAY/REV PAGE MISSION EDITION DATE S503/103 FINAL ovember __22, ...„.... 1968...... ...• •...... 27.:•00 --...... — 2 • s1 1111/Miffill MSC Foim 1910 (Nov 68) FLIGHT PLAN

CDR CMP Liao MCC -H 28:00 -- • • • • V66 TRANS CSM STATE SM RCS MONITOR CK SPS MONITOR CK VECTOR TO LM SLOT TRN BIAS INITIATE BAT CHARGE BIOMED Sw - RIGHT MNVR TO SIGHTING ATT

MCC 2 BURN STATUS REPORT ICISLUNAR NAVIGATION P23I 28:15 - 1. STAR 16 EFH STAR E H 1 SET

2. STAR 22 EFH STAR E H 1 SET

3. STAR 21 EFH STAR E H 1 SET

28:45 — 4. STAR 26 ENH STAR E H 1 SET GROUND TRACK DET P21 MNVR TO PTC ATT P 331 Y 331 CDR CREW STATUS REPORT ROLL 0.1 °/SEC 29:00 ]

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 28:00 - 29:00 2/TLC 2-22 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 0 0 • 0 0 FLIGHT PL AN CDR CMP LMP MCC— H 29:00 LiOH CANISTER CHG COMM TEST (CARTRIDGE NO. 5 FROM A3 MODE: 4 INTO CANISTER A) 5 6 8 4,2 5.2 4,3 29:30 8.1 1.0 0.5 0,6 1.7 0.8 0,10

S 30:00 F SLEEP PERIOD N (7 HOURS)

30:30 EAT PERIOD I EAT PERIOD

UNSTOW TV CAMERA

31:00 ■ T .•

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 29:00 - 31:00 2/TLC 2-23 MSC Form 1910 (Nov 68) FLIGHT PtANNINC3 BRANCH

FLIGHT PL AN CDR CMP LAW MCC-H 31:00 BIOMED Sw - CENTER

TV 31:30 STOW TV CAMERA

32 :00 SLEEP PERIOD (7 HOURS)

32:30

33:00 1 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 31:00 - 33:00 2/TLC 2-24 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 0 0 • • FLIGHT PL AN

CDR CMP LMP MCC-H 33:00 •

33:15

33:30 SLEEP PERIOD (7 HOURS)

33:45 MNVR TO P52 ATT

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

34:00 — -- " —v -- (coned)

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 33:00 - 34:00 2/TLC 2-25 MSC Form 1910 (Nov 58) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC—H 34:00 -- • TORQUE ANGLES: BIOMED X Sw - RIGHT Y

SCT STAR VISIBILITY TRN BIAS MNVR TO SIGHTING ATT 34:15 - ICISLUNAR NAVIGATION P23

. STAR 16 EFH STAR E H 1 SET

34:30 -" SLEEP PERIOD . STAR 22 EFH (7 HOURS) STAR E H 1 SET

STAR 26 ENH STAR E H 34:45 - 1 SET GROUND TRACK DET P21 MNVR TO PTC ATT P 331 Y 331 1 P Y VOICE RECORD BLOCK DATA ROLL 0.1°/SEC UPDATE: (TLI + 35 HOURS, TLI + BLOCK DATA 44 HOURS, AND FLY BY) 35:00 -.1 • •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 34:00 - 35:00 2/TLC 2-26 MSC Faun 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0 0 FLIGHT PLAN CDR CMP LMP MCC—H 35:00

35:30 SLEEP PERIOD EAT PERIOD EAT PERIOD (7 HOURS)

CMP/LMP CREW STATUS REPORT 36:00 F T N BIOMED Sw - LEFT

36:30 EAT PERIOD SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

37:00

MISSION EDITION DATE TIME • DAY/REV PAGE AS503/103 FINAL November 22,1968 35:00 - 37:00 2/TLC 2-27 MSC Farm 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 37:00 CDR CREW STATUS REPORT

37:30

SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS) S 38:00

38:30

39 : 00-]

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 37:00 - 39:00 2/TLC 2-28 MSC Farm 191C (Nov BB) FLIGHT PLANNING BRANCH • 0 0 • 10 FLIGHT PLAN

CDR CMP LMP MCC—H 39:00

39:3

40:00 SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

40:30

LiOH CANISTER CHANGE (CARTRIDGE NO. 6 FROM A3 INTO CANISTER B) 41:00

MISSION EDITION DATE TIME DAY/REV PAGE A5503/103 FINAL November 22, 1968 39:00 - 41:00 2/TLC 2-29 '11 SC Form 1910 (Nov se) FLIGHT PLANNING BRANCH FLIGHT PLAN

CMP LMP MCC—H CDR I 41:00 •

41:30

M S 42:00 F SLEEP PERIOD SLEEP PERIOD N (7 HOURS) (7 HOURS)

42:30

43:00 ..] •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 41:00 - 43:00 2/TLC 2-30

MSC Form 7910 (Nov 08 ) FLIGHT PLANNING BRANCH 411 0 0 FLIGHT PLAN

CDR CMP LMP MCC —H 43:00 BIOMED Sw - CENTER

43:30 S EAT PERIOD I EAT PERIOD EAT PERIOD N

44:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 43:00 - 44:00 2/TLC 2-31

MSC Form 1910 (Nov 613) ELI FLIGHT PLAN CDR CMP LMP MCC-H 44:00 — • 6 RECORD BLOCK DATA CMP/LMP CREW STATUS VOICE (TLI + 44 HOURS, FLY BY, REPORT UPDATE: PC 2 (QUICK RETURN), BLOCK DATA & PC + 2)

•

44:30 — S F N MNVR TO P52 ATT IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID .11 STAR ANGLE DiFF -- TORQUE ANGLEST— -- X Y

GDC ALIGN TO IMU 45:00 -1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 44:00 - 45:00 2/TLC 2-32 MSC Farm 1910 (Nov 68) FLIGHT PLANNING BRANCH

0 0 • ./' VI. 0 0 • • 0 0 FLIGHT PLAN CDR CMP LMP MCC—H• 45:00 — • • MNVR TO SIGHTING ATT TRN BIAS CISLUNAR NAVIGATION P23

. STAR 33 LNH STAR L H 45:15 - 2 SETS

2. STAR 37 LNH STAR L H 45:30 — 1 SET

45:45 3. STAR 45 LFH STAR L H 1 SET

ti 4. STAR 42 LFH STAR L H 1 SET 46:00-- •

. MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 45:00 - 46:00 2/TLC 2-33 MSC Farm 1910 (Hoy 08) FLIGHT PLANNING BRANCH

BURN STATUS REPORT MCC'S - - :X.X — ! --.ATIG BURN CHART t X X BT 'V gx P or Y ATT. SHUTDOWN RATES DEVIATION TIME RESIDUALS . X X X _ ! MCC(ALL) 10°/SEC 10° B/T +1 SEC TRIM TO 0.2 fps TAKEOVER TAKEOVER X XX'I : ID XXX ily V 9>c V gY V gz . A V C X X :X ; FUEL )CX!Xi OX X X !X !UNBALANCE 'REMARKS:

• 0 0 0 • 0 FLIGHT PLAN LMP MCC —H CDR CMP 6 46:00-• BIOMED Sw - *RIGHT P27 UPDATE: GROUND TRACK DET P21 RECORD MNVR PAD STATE VECTOR TGT LOAD VOICE UPDATE: MNVR PAD 46:15 - V47 TRANS LM STATE VECTOR TO CSM SLOT EXT AV P30

SPS/RCS THRUST P40/41

MNVR TO BURN ATT PIPA BIAS SXT STAR CK CK TRANS TO COUCH

,46:46- EMS AV TEST

GDC ALIGN SM RCS MON CK LOI -22 FIRS 1MCC 3 AV-NOMINALLY ZERO 47:00-- U •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 46:00 - 47:00 2/TLC 2-34 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRANCH FLIGHT PL AN

CDR CMP imm MCC—H 47:00 SM RCS MON CK SPS MON CK MNVR TO SIGHTING ATT INITIATE BAT CHARGE

V66 TRANS CSM STATE VECTOR TO LM SLOT BURN STATUS REPORT MCC i TRN BIAS 47:15 ICISLUNAR NAVIGATION P231 1. STAR 16 EFH STAR E H 1 SET

47:30 2. STAR 22 EFH STAR E H 1 SET

3. STAR 26 ENH STAR E H 1 SET 47:45 MNVR TO PTC ATT P 331 Y 331 GROUND TRACK DET P21 ROLL 0.1°/SEC

48: 00—

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 47:00 - 48:00 2/TLC 2-35 MSC Form 1910 (Nov 90 FLIGHT PLANNING BRANCH 0 • • 0 0 FLIGHT PLAN LMP MCC—H CDR CMP ti 48:00 — • •

48:30 -

S BIOMED Sw - CENTER 49:00- F N

49:30 - EAT PERIOD EAT PERIOD I EAT PERIOD

50:00—

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 48:00 - 50:00 3/TLC 2-36 MSC Form 1910 (Nov 613) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC—H 50:00

50:30

S 51:00 RECORD BLOCK DATA VOICE (FLY BY & PC 2 HOURS) UPDATE: BLOCK DATA

51:30 MNVR TO P52 ATT

IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF CDR CREW STATUS REPORT (cont'd) 52:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 50:00 - 52:00 3/TLC 2-37 MSG Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 • r) fr •

FLIGHT PL AN LMP MCC-H CDR CMP 52:00 TORQUE ANGLES: 3IGMED Say - • RIGHT X Z —

TRANS TO LH COUCH MNVR TO SIGHTING ATT GDC ALIGN TO IMU 52:15 TRN BIAS 1CISLUNAR NAVIGATION P23

1. STAR 37 LNH STAR L H 2 SETS 52:30 — S F SLEEP PERIOD N (7 HOURS)

2. STAR 33 LNH STAR L H 52:45 — 3 SETS

••■

53:00 —

TIME DAY/REV PAGE MISSION EDITION DATE AS503/103 FINAL November 22,1968 52:00 - 53:00 3/TLC 2-38 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC-H 53:00 • •

53:15 GROUND TRACK DET P21 MNVR TO PTC ATI P 331 Y 331 P Y ROLL 0.1°/SEC

53:30 SLEEP PERIOD (7 HOURS)

53:45

54:00 -I 4

MISSION EDITION DATE TIME DAY! RAI , PAGE AS503/103 FINAL November 22,1968 53:00 - 54:00 3/TLC 2-39 , MSC Form 1910 (Noy 68) FLIGHT PLANNING BRANCH • 0 ill 0• 410 0 0

FLIGHT PL AN CMP LMP MCC—H CDR • 54:00 •

54:15

1'4 S 54:30 F SLEEP PERIOD (7 HOURS)

54:45

BIOMED Sw - CENTER UNSTOW TV CAMERA 55:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 54:00 - 55:00 3/TLC 2-40 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRAN

FLIGHT PLAN

CDR CMP LMP MCC—H S 55:00 --

• 55:15- , 1 T V

1 55 :30 — S SLEEP PERIOD F (7 HOURS) N STOW TV CAMERA

55:45-

56:0 0] •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 55:00 - 56:00 3/TLC 2-41 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 0 0 • FLIGHT PLAN CDR CMP LMP MCC—H 56:00 •

56:30 EAT PERIOD EAT PERIOD

5 57:00 F SLEEP PERIOD N (7 HO RS)

57:30

58:0 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 56:00 - 58:00 3/TLC 2-42 MSO Form 1910 (Nov 88) FLIGHT PLANNING BRANCH FLIGHT PL AN

CDR CMP LMP MCC—H 58:00

58:30 SLEEP PERIOD (7 HOURS)

59:00 SIOMED Sw - LEFT

59:30 EAT PERIOD P27 UPDATE: STATE VECTOR TGT LOAD REFSMMAT VOICE UPDATE RECORD MNVR PAD MNVR PAD CDR CREW STATUS REPORT 60:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 58:00 - 60:00 3/TLC 2-43

MSC Form 1810 (Nov 68) FLIGHT PLANNING BRAN

0 •

MCC'S BURN STATUS REPORT BURN CHART X x 11 ATIG X x BT V P or Y ATT SHUTDOWN El . gx RATES DEVIATION TIME RESIDUALS TRIM_ X X X MCC(ALL) 10°/SEC 10° B/T +1 SEC TRIM TO 0.2 fns TAKEOVER TAKEOVER IX X X !XXX V • gx gY V gZ 6V C X X X FUEL X X X Ox

X X X . UNBALANCE REMARKS: FLIGHT PLAN

CDR CMP LMP MCC —H 60:00— • 6 MNVR TO P52 ATT

IMU REALIGN P52 OPTION 1 - PREFERRED STAR ID 60:15- STAR ANGLE DIFF TORQUE ANGLES: X

Z

60:30— EXT AV P30 SPS/RCS THRUST P40/41 MNVR TO BURN ATT

SXT STAR CK PIPA BIAS CK EMS AV TEST 60:45 ,— TRANS TO COUCH

GDC ALIGN TO IMU SM RCS MON CK MCC AV =. NOMINALLY ZER 61:00 4

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 60:00 - 61:00 3/TLC 2-44 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • FLIGHT PLAN

CDR CMP LMP MCC—H 61:00 I SM RCS MON CK V66 TRANS CSM STATE SPS MON CK VECTOR TO LM SLOT GROUND TRACK DET P21 INITIATE BAT CHARGE (STATE VECTOR CK) ECS REDUNDANT COMP CK MNVR TO PTC ATT P 122 Y 315 P Y 61:15 ROLL 0.1 °/SEC

S 61:30 F N

61:45

CMP/LMP CREW STATUS REPORT 62:00 - • •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November p2,1968 61:00 - 62:00 3/TLC 2-45 MSC Form 1910 (Nov 68) LFOGHTPLANNINGBRANCH FLIGHT PL AN

CDR CMP LMP MCC—H 62:00 a

62:30

H SLEEP PERIOD SLEEP PERIOD 63:00 (6 HOURS) (6 HOURS)

63:30

64:00 -1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 62:00 - 64:00 3/TLC 2-46 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 • FLIGHT PL AN

CDR CMP LMP MCC—H 64:00

64:30

S 65:00 F SLEEP PERIOD SLEEP PERIOD (6 HOURS) (6 HOURS)

65:30

MNVR TO P52, ATT 66 : 00

MISSION EDITION DATE TIME DAY/REV PAGE AS603/103 FINAL November 22,1968 64:00 - 66:00 3/TLC 2-47 MSC Form 19I0 (Nov Eli) FLIGHT PLANNING BRANCH

FLIGHT PLAN

CDR CMP LMP MCC —H 66:00 • IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF TORQUE ANGLES: X 66:15 Y

GDC ALIGN TO IMU MNVR TO PTC ATT P 122 Y 315

66:30 ROLL O. 17YE0 SLEEP PERIOD SLEEP PERIOD (6 HOURS) (6 HOURS)

RECORD MNVR PAD FOR LOI 1 VOICE UPDATE: MNVR PAD 66:45

67:00-1

DATE TIME DAY/REV PAGE MISSION' EDITION _ AS503/103 FINAL November 22,1968 66:00 - 67:00 3/TLC 2-48 MSc Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0 0 0 0 11 FLIGHT PLAN

CDR CMP LMP MCC—H • 67:00 -- ATT MNVR TO LOI 1 SXT STAR CK

MNVR TO PTC ATT P 122 V 315 P ROLL 0.1c/SEC 67:15' RECORD BLOCK DATA VOICE (TEI TEI & PC+2) 1' 2' UPDATE: BLOCK DATA & MAP UPDATE & MAP UPDATE 1/2

67:30 — SLEEP PERIOD SLEEP PERIOD (6 HOURS) (6 HOURS)

67:45 —

68:00--

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 67:00 - 68:00 3/TLC 2-49 MSC Form 1610 (Nov 68) FLIGHT PLANNING BRANCH

FLIGHT PL AN

CDR CMP L MP MCC-H • 6 68:00 • GO/NO GO FOR LOI 1 CMP/LMP CREW STATUS GO/NO GO REPORT GROUND TRACK DET - P21 P27 UPDATE: STATE VECTOR (LOI ALTITUDE DET) RECORD MANEUVER PAD TARGET LOAD

MNVR TO P52 ATT VOICE UPDATE: MNVR PAD IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIF --

TORQUE ANGLES: PRE LOI SYSTEMS CKS: X C&W CK CM RCS CK 68: 30 — SM RCS CK SPS PERIODIC MONITOR EPS PERIODIC MONITOR EXTERNAL AV P30 ECS PERIODIC MONITOR EMS CK SPS THRUST P40 MNVR TO BURN ATT SXT STAR CK TRANSFER TO COUCH

GDC ALIGN TO IMU

68:57 69:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 68:00 - 69:00 3/TLC 2-50 MSC Form 1910 (OT) (Oct 68 ) FLIGHT PLANNING BRANCH • 1111 •- di111 0 •

BURN STATUS REPORT LOI X X ATIG 1 BURN CHART X X BT V P or Y ATT SHUTDOWN RESIDUALS gx RATES DEVIATION TIME TRIM - X X X R 10°/SEC 10° B/T+6 SEC NO TRIM LOI 1 TAKEOVER TAKEOVER X X X P MODES X X X LO1 1 ABORT na V gx LOI BST TRAJECTORY ABORT MODE ■_71 V90 0 • v gY 3050-2100 0 -1:20 HYPERBOLIC COAST OUT OF SPHERE-P37 V 2100-1650 1:20-2:00 UNSTABLE 5 HR COAST. MODE I ABORT • gz 1650-0 2:00-4:06 LUNAR ORBIT MODE III ABORT AFTER AV C 1 REV X X X FUEL X X X ox X X X UNBALANCE REMARKS: FLIGHT PLAN

CDR CMP LMP MCC-H 69:00 -- • • • BIOMED Sw - CENTER SM RCS MONITOR CK

LOT GETI = 69:07:30 1 AV = 2991 fps BEGIN BT = 4 MIN 5:8 SEC REV 1 ' GDC ALIGN TO IMU/ORB V66 TRANS CSM STATE SPS MONITOR CK RATE (115 nm) VECTOR TO LM SLOT GO INERTIAL SM RCS MONITOR CK INITIATE BAT CHARGE CAMERA PREP ROLL RIGHT 180 0 AT 2°/SEC,_CONT INERTIAL 2/80/83 4. 1/150/A8, ATT HOLD R&B FILTER/U4, SPOT/ 69:3 R13,INT/U4, 2 B&W FILM V64 ACQUIRE MSFN ON HGA ACQUIRE S/C BURN STATUS REPORT LOI 1 PACKS 1A8 UNSTOW ORBITAL CHARTS, DUMP DSE 16/18/NEW C-EX/CABLE/ BRKT/U3 2/150/NEW B&W 1/250 16/18/NEW C EX, 1/250, 2/80/NEW B&W SPOT, 1 FPS, (1 MAG) 1/80/B&W, 1/250 M PIPA BIAS S CK N

EAT PERIOD EAT PERIOD EAT PERIOD

• 70:00 --

PAGE MISSION EDITION DATE TIME DAY/REV 3/LPO 2-51 ASU3/103 FINAL November 221 196E, 69:00 - 70:00 MSC Farm 1910 (Nov 08) FLIGHT PtANNI • 0 • • • 0 0 FLIGHT PLAN CDR CMS' LMP MCC—H I

EAT PERIOD

1/50/HS, 1/4 VERIFY IMU REALIGN P52 F 2.8 SYSTEMS OPTION 3 - REFSMMAT STATUS AND GYRO DRIFT TEST STAR ID EAT PERIOD STAR ANGLE DIF -- -- EAT PERIOD TORQUE ANGLET UNSTOW TV CAMERA & BRKT & TELEPHOTO LENS (A) TEMP STOW INT

GDC ALIGN TO IMU RECORD BLOCK DATA VOICE (TEI 1 & TEI) UPDATE: EAT PERIOD BLOCK DATA

PITCH UP TO PREPARE AND REVIEW CNTL 1/80/B&W, 1/250, F 2.8, ORDEAL 180, 315, 0 AT POINT AND LDMK CHARTS INT 0.2°/SEC (HEADS DWN COAS 1/150/B&W

TRACK ATT) BEGIN ORB RAT : 2/150/B&W, 1/250, F 2.8

16/18/NEW C EX, 1/250, F 2.8, 1 fps (1 MAG) •

MISSION EDITION DATE TIME DAY /REV PAGE AS503/103 FINAL November 22, 1968- 70:00 - 71:00 3/LPO 2-52 MSC Form 1916 (Nov 88) FLIGHT PLANNING BRANCH

FLIGHT PLAN

CDR CMP LMP MCC—H • I CONTROL PT (CP) SIGHTING (THRU HATCH WINDOW) MAINTAIN ORB RATE AND START 16 MM CAMERA BEGIN COAS GROUND TRACK AT TERMINATOR DETERMINATION CP1 7 1 : 1 3: 4 6 TCA SPOT METER READINGS CP1 NO. 504 PHOTOGRAPH TARGETS LAT -05.250°S OF OPPORTUNITY LONG -162.700°W ALT 000.00 nm

CP2 7 1: 2 7 : 4 0 TCA CP2 NO. 526 LAT -10.200°S CONFIGURE FOR TV LONG +155.100°E ALT 000.00 nm YAW RT 45° FOR TV ORDEAL 180, 315, 45

V64 ACQUIRE MSFN ON HGA CP3 7 1: 4 6: 3 8 ACQUIRE S/C TCA CP3 NO. 334 P27 UPDATE: TV LAT -09,100°S STATE LONG +95.900°E VECTOR ALT 000 -.00 nm TARGET LOAD

YAW LEFT 45° TO I ORDEAL 180, 315, 0 RECORD MAP UPDATE VOICE PSEUDO LDG SITE LDMK UPDATE: SIGHTING (THRU HATCH MAP UPDATE WINDOW) 2/3 72:00

MISSION EDITION DATE TIME DAY/REV PAGE 2-53 AS503/103 FINAL November 22, 1968 71:00 - 72:00 3/LPO MSC Form 1810 (Nov 68) FLIGHT PLANNING BRANCH

0 • 0

FLIGHT PLAN

CDR CMP LMP MCC-H 72:00 MAINTAIN ORBITAL RATE B-1 7 2: 0 9 : 1 0 AND COAS GROUND TRACK TCA1 DETERMINATION LDMK NO. B1 LAT +02,675°N 72:10 LONG +35.025°E ALT -000.99 nm BIOMED Sw - LEFT GO/NO GO FOR L01 2 LiOH CANISTER CHANGE STOP 16 MM CAMERA GO/NO GO (CARTRIDGE 9 FROM 85 RECORD MNVR PAD, BLOCK VOICE INTO CANISTER A) DATA (TEI 3 , TEI 3 NO UPDATE: LO1 ) MNVR PAD 72:23 2 BLOCK DATA

72:30 — IMU REALIGN P52 DUMP DSE OPTION 3 - REFSMMAT 1/80/HS, 1/4, F 2.8 AND GYRO DRIFT TEST STAR ID , STAR ANGLE RIFF TORQUE ANGLES: — PRE LOI SYSTEMS CKS: X PIPA BIAS z _ C&W CK CK CM RCS CK • SPS PERIODIC MONITOR EXTERNAL AV P30 EPS PERIODIC MONITOR ECS PERIODIC MONITOR EMS CK SPS THRUST - P40 • 73:00 -- •

MISSION EDITION DATE TIME DAY/REV PAGE AS503 103 FINAL November 22, 196: 72:00 - 73:00 4/LPC 2-54 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH LOI 2 BURN STATUS REPORT ---; - 1-- - I BURN CHART !X X. " 1ATIG )

V • , gx 1V 3 gY V gz

AV C FUEL j)); :UNBALANCE REMARKS:

0 0 0 0 • 0 • FLIGHT PLAN CDR CMP LIMP MCC—H b 73:00 -- • 2/80/B&W, 1/250 73:03 • MNVR TO BURN ATT GO INERTIAL SXT STAR CK 16/18/C EX, 1/250 F CHART, 6 fps, BRACK TRANSFER TO COUCH 73:09 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 SPS MONITOR CK REV 3 GDC ALIGN TO IMU/ORB RATE (60 nm) V66 TRANS CSM STATE VECTOR TO LM SLOT ROLL RIGHT 180° AT SM RCS MONITOR CK INITIATE BAT CHARGE 2°/SEC PITCH DWN AT 0.2°/SEC (HEADS OWN TRACKING ATT) ORDEAL 180, 308, 0 BEGIN ORB RATE ACQUIRE S/C 73:48 V64 ACQUIRE MSFN ON HGA LOI 2BURN STATUS REPORT PIPA BIAS REST PERIOD CK (2 HOURS)

BIOMED Sw - RIGHT 74:00

MISSION EDITION DATE TIME DAY/REV PAGE 74:00 4/LPO 2-55 AS503/103 FINAL November 22, 1962 73:00 - 1 MSC Fun 1910 (Nov 69) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H • • TRAINING PHOTOGRAPHY 'TRAINING PHOTOGRAPHY ,70mm & 16mm

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 5 :

74:17 STOP CAMERA STOP CAMERAS PITCH DWN TO HEADS DWN 1/80/HS, 1/4, F 2.8 TO REACQUIRE MSFN ORDEAL 180, 0, 0 VOICE GO INERTIAL VERIFY SYSTEMS STATUS UPDATE: REST PERIOD RECORD MAP UPDATE MAP UPDATE (2 HOURS) 3/4 DUMP DSE IMU REALIGN P52 OPTION 3 REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF TORQUE ANGLES: X Y INSTALL 16 MM CAMERA I GDC ALIGN TO IMU RECORD BLOCK DATA VOICE (TEI 3 & TEI 4 ) UPDATE: BLOCK •DATA 75:00 =I • r"-^",„,,o a

DAY/REV PAGE MISSION EDITION DATE TIME 2-56 74:00 - 75:00 4/LPO AS5L3/103 LINAI November 22, 1968 MSC Form 1810 (Nov 88) FLIGHT PLANNI FLIGHT PL AN LMP MCC—H CDR CMP U 75:00 • PITCH UP TO VERTICAL AT 1/80/NEW B&W, 1/250, 0.2°/SEC (+Z FWD) F 2.8 BRKT/INT ORDEAL 180, 270, O. BEGIN ORB RATE 2/150/B&W 75:09 16/18/NEW C EX/1 fps 1/250, F 2, 1 fps START CAMERA S/S SR 4- 75:15 6 MIN START CAMERA 1 S/C SR 6 MIN

VERTICAL STEREO PHOTOGRAPHY EXTRA EXP EACH 5 MIN - NOTE TIME 75:30 REST PERIOD (2 HOURS) BEGIN REV 4

SUBSOLAR POINT

75:46 ROLL RIGHT 180° AT INSTALL SXT BRKT & 75:46 2°/SEC (-Z. FWD) 16mm CAMERA. TAKE MAINTAIN ORB RATE PHOTOS AS TIME PERMITS, ACQUIRE ACQUIRE S/C MSFN ON QMNI ANT SA 0° TA 0 °

76:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 75:00 - 76:00 4/LPO 2-57 MSC Form 1910 (Nov 68) FLIGHT PLAMNING BRANCH

FLIGHT PLAN

CDR CALF LMP MCC-H 76:0 T PITCH UP AT 0.2°/SEC AT PITCH UP 1/80/B&W, TO 0, 35, 5, 0 IPI . 1/250, F 11 ACQ •. . . IPII . .

BEGIN ORB RATE ACQ •. . {LDMK LIGHTING EVALUATION STOP CAMERAS AT (THRU OPTICS) OF LDMK 81 STOP CAMERA 1 AT TERM 76:15 TERMINATOR RECORD MAP UPDATE VOICE UPDATE: 76:21 MAP UPDATE 4/5 P27 UPDATE: STATE VECTOR ROLL RIGHT 180° AT 76:30 —1 2°/SEC (HEADS DWN) V64 ACQUIRE MSFN ON HGA ACQUIRE S/C GO INERTIAL IMU REALIGN P52 OPTION 3 - REFSMMAT 1/80/HS, 1/4, F 2.8 S AND GYRO DRIFT TEST '(20 SEC STRIP - 20 EXP) DUMP DSE F STAR ID STAR ANGLE DIFF, — -- VERIFY SYSTEMS STATUS RECORD BLOCK DATA: TORQUE ANGLE S : VOICE X (TEI 4 & TEI 5 ) UPDATE: Y BLOCK DATA TRANS TO LEFT COUCH Z . EAT PERIOD 1 GDC ALIGN TO IMU 1/80/B&W, 1/250, F 2.8 INT (CDR). 76:58 BIOMED Sw - CENTER 77:00

MISSION EDITION DATE TIME DAY/ REV PAGE 4/LPO 2-58 AS503/103 FINAL November 22, 1968 76:00 - 77:00 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0

FLIGHT PLAN LMP MCC -H CDR CMP ti 77:00 • ROLL LEFT 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC TO MAP REVIEW ORDEAL 0, 5, O. BEGIN 77:08 ORB RATE. 2/150/B&W, 1/250 F 2.8

77:14 P22 MANUAL ACQ SA 0°, TA 10°

EAT PERIOD I CNTL POINT SIGHTING

BEGIN IP I REV 5 ACQ 2/150/B&W, 1/250 (CDR) 77:30 CP2 NO. 526 PITCH DWN AT 0.3°/SEC LAT -10.200°S AT ACQ LONG/2 +77.550 ° +000.00 ALT nm NEW COORDINATES LAT LONG/2 ACQUIRE S/C 77:44 ALT nm ACQUIRE MSFN ON OMNIS AT LOSS PITCH UP AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN REST PERIOD ORB RATE. (3 HOURS) REVIEW LDMK MAP REPORT NEW CP COORDINATES

78:00

MISSION EDITION DATE TIME DAY/REV PAGE 2-59 AS503/103 FINAL November 22, 1968 77:00 - 78:00 4/LPO MSC Form 1910 (Nov 88) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H • 6 PSEUDO LDG SITE SIGHTINGS P22 - AUTO OPTICS IPI TCA PITCH DWN 0.3°/SEC AT ACQ LDMK NO, 81 AT LOSS ROLL RIGHT 180° LAT +02.675°N AT 2°/SEC TO HEADS DWN LONG/2 +17.512° GO INERTIAL ALT -000.99 nm NEW COORDINATES LAT + LONG/2 + 0 V64 ACQUIRE MSFN ON HGA ACQUIRE S/C ALT n 1/80/HS, 1/4, F 2.8 P27 UPDATE: REPORT NEW COORDINATES STATE VECTOR RECORD BLOCK DATA VOICE REST PERIOD (TEI 6 ), & MAP UPDATE UPDATE: (3 HOURS) BLOCK DATA IMU REALIGN P52 VERIFY SYSTEMS STATUS MAP_ OPTION 3 - REFSMMAT UPDATE AND GYRO DRIFT TEST 5/6 STAR ID STAR ANGLE DIFF-- TORQUE ANGLES: DUMP DSE 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 EDITION DATE TIME DAY/REV PAGE - 79:00 4/LPO 2-60 AS503/103 FINAL Novemb e r 22, 1968 78:00 MSC Form 1910 (Nov 68) FLIGHT PLAN

• 0 ti • 0 0 • 1 0 FLIGHT PLAN LMP MCC—H CDR CMP S 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]

P22 - AUTO OPTICS IPI TCA CP2 NO. 526 LAT -10.200°S LONG/2 +77.550° REST PERIOD ALT +000.00 nm PITCH DWN 0.3°/SEC AT AC (3 HOURS) NEW COORDINATES LAT 0 T LOSS PITCH UP AT LONG/2 0.2°/SEC TO ALT nm 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 EDITION DATE TIME DAY/REV PAGE 4/LPO 2-61 AS503/103 FINAL November 22, 1968 79:.00 - 80:00 MSC Form 1910 (Nov Ea) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LPAP MCC—H 80:00 • P22 AUTO OPTICS IPII TCAI LDMK NO. B1 LAT +02.675°N PITCH DWN 0.3°/SEC AT ACQ LONG/2 +17.512° ALT -000.99 nm 80:13 NEW COORDINATES LAT 0 AT LOSS ROLL RIGHT 180° LONG/2 AT 2°/SEC. GO INERTIAL 0:19 ALT nm V64 ACQUIRE MSFN ON HGA ACQUIRE S/C REST PERIOD P27 UPDATE: (3 HOURS) REPORT NEW COORDINATES STATE VECTOR RECORD BLOCK DATA VOICE (TEI 7 )& MAP UPDATE UPDATE: BLOCK DATA IMU REALIGN P52 & MAP OPTION 3 - REFSMMAT UPDATE 6/7 AND GYRO DRIFT TEST VERIFY SYSTEMS STATUS DUMP DSE STAR ID , 1/80/B&W, 1/250 F 2.8 IN STAR ANGLE DIFF 2/150/B&W, 1/250 (R&B) TORQUE ANGLET— -- Xy TRANS TO RIGHT COUCH

ROLL LEFT 180° AT EAT PERIOD 2°/SEC PITCH UP AT 0.2°/SEC TO 16/SXT/NEW C XT, ORDEAL 0, 5, O. BEGIN 6 fps ORB RATE

MISSION EDITION DATE TIME DAY/REV f PAGE 2-62 AS503/103 FINAL November 22, 1968 80:00 - 81:00 4/LPO MSC Form 1910 (Nov 88) FLIGHT PLANNING H

• 0 14 , 0 • 0 • FLIGHT PLAN MCC—H CDR CMP LMP 81:00-- LEFT ICNTL PT SIGHTINGS (3)1 BIOMED Sw -

81:05 - EAT PERIOD P22 MAN ACQ SA 0° TA 10° 81:11 - IPI PITCH DWN AT 0.3°/SEC AT ACQ ACQ CP1 NO. 504-- -- NEW COORDINATES AT LOSS PITCH UP AT LAT -05.250°S LAT 0 0.5°/SEC TO LONG/2 -81.350° LONG/2 ORDEAL 0, 5, 0 ALT +000.00 nm ALT nm P22 AUTO OPTICS T IPI I EAT PERIOD TCA 1 ' -- PITCH DWN AT 0.3°/SEC AT CP2 NO. 526 NEW COORDINATES ACQ LAT -10.200°S LAT LONG/2 +77.550 ° LONG/2 T LOSS PITCH UP AT ALT +000.00 nm ALT nm 0.5°/SEC TO RDEAL 0, 5, 0

P22 MAN ACQ SA 0° TA 10° IPI I ACQUIRE 5/C ACQ I •. CP3 NO. 334 - NEW COORDINATES PITCH OWN AT 0.3°/SEC AT LAT -09.100°S LAT CQ LONG/2 +47.950° LONG/2 . ° ALT +000.00 nm ALT nm

AT LOSS PITCH UP AT 0.5°/SEC TO 'PSEUDO LOG SITE SIGHTING' ORDEAL 0, 5, 0 P22 AUTO OPTICS

PAGE MISSION EDITION DATE TIME DAY/REV - 82:00 4/LPO 2-63 AS503/103 FINAL November 22, 1968 81:00 MSC Form 1910 (Nov 68) FUG

FLIGHT PLAN

CMP LMP MCC—H 82:00 — • IP I TCA PITCH DWN AT 0.3°/SEC LDG SITE NO. B1 AT ACQ LAT +02.675°N LONG/2 +17.512° 82:11 AT LOSS ROLL RIGHT 180° ALT -000.99 nm AT 2°/SEC NEW COORDINATES GO INERTIAL LAT 82:17 LONG/2 0 ACQUIRE MSFN ON HGA ALT nm ACQUIRE S/C REPORT NEW COORDINATES P27 UPDATE: STATE RECORD MAP UPDATE & VECTOR BLOCK DATA (TEI 8 ) VOICE UPDATE: IMU REALIGN P52 REST PERIOD MAP UPDATE (2 HOURS) 8 OPTION 3 - REFSMMAT BLOCK DATA 82:30 — AND GYRO DRIFT TEST STAR ID DUMP DSE STAR ANGLE JIF !F -- TORQUE ANGLES: X Y Z

GDC ALIGN TO IMU

ROLL LEFT 180° AT 2°/SEC TO HEADS UP 82:53 — I

16/SXT/CXT„6 fps 83:00 • I

MISSION EDITION DATE TIME DAY/REV PAGE 2-64 AS503/103, FINAL November 22, 1968 82:00 - 83:00 4/LPO MSC Form 1910 (Nov 08) FLIGHT PLANNI 0 0 0 0 0 • • 0 FLIGHT PLAN LMP MCC-H CDR CMP ti 3:00 PITCH DWN AT. 0.2°/SEC TO ICNTL PT SIG}-TINGS (3) ORDEAL 0, 5, 0 REST PERIOD 83:03 P22 AUTO OPTICS (2 HOURS) 11)1 __. .._, __ __ TCA CP1 NO. 504 NEW COORDINATES 83:10 LAT -05.250°S LAT PITCH DWN AT 0.3°/SEC LONG/2 -81.350° LONG/2 AT ACQ ALT +000.00 nm ALT nm

AT LOSS PITCH UP AT P22 AUTO OPTICS 0.5°/SEC TO IPI . ORDEAL 0, 5, 0 TCA •. EGIN CP2 NO. 526 NEW COORDINATES REV 8 LAT -10.200 ° S LAT LONG/2 +77.550° LONG/2 0 PITCH OWN AT 0.3°/SEC ALT +000.00 nm ALT nm AT ACQ 83:30 PITCH UP AT 0.5 ° /SEC TO ORDEAL 0, 5, 0 P22 AUTO OPTICS IPII 83:39 ACQUIRE S/C TCA • ACQUIRE MSFN ON OMNIS . CP3 NO. 334 NEW COORDINATES LAT • -09.100°S LAT LONG/2 +47.950 ° LONG/2 0 PITCH OWN AT 0.3°/SEC ALT +000.00 nm ALT nm AT ACQ

PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0 PSEUDO LOG SITE SIGHTINGI

P22 AUTO OPTICS 84:00 •

MISSION EDITION DATE TIME DAY, REV PAGE 84:00 4/LPO 2-65 AS503/103 FINAL November 22, 1968 83:00 - MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CMP LMP MCC—H 84:0 • I IPI I TCA PITCH DWN AT 0.3°/SEC LDMK NO. 81 NEW COORDINATES AT ACQ LAT +02.512°N LAT LONG/2 +17.512° LONG/2 84:10 ALT +000.99 nm ALT nm AT LOSS ROLL RIGHT 180° AT 2°/SEC (HEADS DWN) REST PERIOD GO INERTIAL 84:16 (2 HOURS) ACQUIRE MSFN ON HGA LION CANISTER CHANGE 1 ACQUIRE S/C (CARTRIDGE 10 FROM B5 2/150/NEW B&W, 1/250 INTO CANISTER B) (R&B) P27 UPDATE: STATE BIOMED Sw - RIGHT VECTOR IMU REALIGN P52 OPTION 3 - REFSMMAT VERIFY SYSTEMS STATUS DUMP DSE 84:30 — AND GYRO DRIFT TEST STAR ID , _ VOICE STAR ANGLE DIFF UPDATE: MAP UPDATE TORQUE ANGLES: 8/9 X BLOCK DATA RECORD MAP UPDATE & z BLOCK DATA (TEI 9 ) DC ALIGN PITCH UP AT 0.2°/SEC TO 1/80/H.S. B, f2.8, POL ORDEAL 180, 0, 0 (HEADS 84:51 DWN) BEGIN ORB RATE REST PERIOD SR -12 MIN START DARK (2 HOURS) 1/80 B&W, 1/4, f4,POL 16/18/NEW CEX, 1/250, SR -4 MIN START CORONA f2.8, 1 fps 85: 00 -I • •

MISSION I DITION DATE TIME DAY/REV PAGE 2-66 AS503/103 FINAL November 22, 1968 84:00 - 85:00 4/LPO MSC Form 1910 (Nov 58) FLIGHT PLANNING BRANCH • 0 0 • ,4r FLIGHT PL AN CDR CMP LMP MCC—H 85:00 • • • 85:0 AT S/C SR 1/80/NEW C BRKT INT PITCH UP 60° AT 0.5°/SEC` TO ORDEAL 180, 300, 0 CONTINUE ORB RATE 85:08 START CAMERA AT S/C SR +12 MIN START CAMERA I AT SR +12 MIN

ZERO PHASE TARGETS OF BEGIN OPPORTUNITY REV 9 CONVERGENT STEREO PHOTOGRAPHY-EXTRA 85:30 EXP EACH 5 MIN - NITE TIME

REST PERIOD (2 HOURS) ACQUIRE MSFN ON HGA ACQUIRE S/C 85:3 PITCH UP 40° AT 0.2°/SEC TO ORDEAL 180, 260, 0 RECORD MAP UPDATE VOICE UPDATE: ] MAP UPDATE ROLL RT AS REQD TO SHADE 9/10 WINDOWS-KEEP X-AXIS +10° ON TRACK

TV 2/80 B&W/R&B 4 STOPS WIDER

86: 00

MISSION EDITION DATE TIME DAY/REV PAGE 4/LF0 2-67 AS503/103 FINAL November 22, 1968 85:00 - 86:00 MSC Farm 1910 No 6 8) FLIGHT PL N I FLIGHT PLAN

CDR CMP LMP MCC—H • ri I

STOP CAMERA AT TERM REST PERIOD STOP CAMERA AT TERM (2 HOURS) 2/80/HS, 1/4 f2.8

ROLL RIGHT 180° IF REQD P27 UPDATE: PITCH DWN 60° AT STATE 0.2°/SEC TO VECTOR ORDEAL 180, 310, 0 (HEADS DWN) GO INERTIAL RECORD BLOCK DATA VOICE (TEI 10 ) & MNVR PAD UPDATE: BLOCK DATA MNVR PAD

IMU REALIGN P52 DUMP DSE I OPTION 3 - REFSMMAT AND GYRO DRIFT TEST VERIFY SYSTEMS STATUS STAR ID , STAR ANGLE DIFF TORQUE ANGLEST----- x Y

PITCH DWN AT 0.2°/SEC TO ORDEAL 180, 180, 0 BEGIN ORB RATE 1/80/NEW B&W 1/250, (HEADS DWN +Z FWD) f2.8 INT (CDR) 2/150/C, 1/250 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL i November 22, 1968 86:00 - 87:00 4/LPO 2-58 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0 • FLIGHT PLAN

CDR CMP LMP MCC—H • •

MNVR TO TEI ATT SXT STAR CK

BEGIN PITCH UP AT 0.2°/SEC TO REV 10 ORDEAL 180, 180, 0 BEGIN ORB RATE

EAT PERIOD EAT PERIOD EAT PERIOD

2/150/B&W OR 0,1/250 ACQUIRE S/C ACQUIRE MSFN ON HGA DUMP DSE PIPA BIAS CK P27 UPDATE: STATE VECTOR TARGET LOAD RECORD MNVR PAD, BLOCK VOICE DATA (TEI 11 ), MAP UPDATE UPDATE: MNVR PAD BLOCK DATA - 1' MAP UPDATE 10

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 87:00 - 88:00 4/LPO 2-69 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 88:00 — • GO/NO GO FOR TEI BIOMED Sw - GO/NO GO LEFT

88:07

88:13 IMU REALIGN P52 2/150/C SPOT OPTION 3 - REFSMMAT 16/75/CEX/1 fps/SPOT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF PRE TEI SYSTEMS CKS TORQUE AGES C&W CK CM RCS CK 88:30 — Y SM RCS CK SPS PERIODIC MONITOR EXTERNAL AV P30 EPS PERIODIC MONITOR EMS TEST ECS PERIODIC MONITOR SPS THRUST P40 MNVR TO BURN ATT

SXT STAR CK PUGS MODE Sw - AUX TRANSFER TO COUCH

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 88:00 - 89:00 _ 4/LPO 2-70 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH

• • (4 0 0

TEI BURN STATUS REPORT BURN CHART X I X ATIG P or Y ATT SHUTDOWN RESIDUALS X X BT RATES DEVIATION TIME •t V 10 ° /SEC 10° B/T+2 SEC & gx TEl TRIM TO 2,0 fps TAKEOVER TAKEOVER AV -40 fps T RIM c >XXi TEI ABORT MODES-SYSTEMS PROBLEMS:15-MIN ABORT CHART OTHERWISE 1 XI X X TEI V qo B/T TRAJECTORY ABORT MODE )()<>0 ! IY 2850-950 0 -2:00 LUNAR ORBIT MODE III AFTER 1 REV V gx 950-600 2:00-2:20 UNSTABLE 5-HR COAST, MODE I V 600-0 2:20-2:54 HYPERBOLIC COAST OUT OF SPHERE - P37 gY t T-V gz

C X XIX FUEL X X A Xti . !Ox 'X X:Xi - 'UNBALANCE REMARKS:

FLIGHT PLAN

CDR CMP LMP MCC—H 89 : 0 0 • • •

SM RCS MON CK

GDC ALIGN TO IMU GETI = 89:15:07 AV = 3532 fps 89:76 - iTEII BT = 3, MIN 26 SEC

PITCH UP TO VERTICAL SM RCS MON CK SPS MON CK +Z FWD) TO ACQ MOON IN WIND W ACQUIRE MSFN WITH HGA CDR CREW STATUS REPORT ACQUIRE S/C TRANS CSM STATE VECTOR TEI BURN STATUS REPORT TO LM SLOT INITIATE BAT CHARGE

89:30 — REINITIALIZE W MATRIX R +00094 BIOMED Sw - CENTER 1 R 2 +00571 R 3 +00003 SLEEP PERIOD ml (5 HOURS)

89:45 - I DUMP DSE UPDATE ENTRY REFSMMAT 90:00 :I • •

MISSION EDITION DATE TIME DAY/ REV PAGE AS503/103, FINAL November 22, 1968 89:00 - 90:00 4/TEC 2-71 MSC Form 1310 (Nov 68) FLIGHT PLANNING BRANCH 4I) • 4D 0 0 • 0 FLIGHT PLAN

CDR LMP LMP MCC— H 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 TRN BIAS (5 HOURS) MNVR TO SIGHTING ATT LCISLUNAR NAVIGATION P231 1. STAR 01 LNH STAR L H 2 SETS —

90:45 -

2. STAR 02 LNH STAR L H

91:00 -- • •

, MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 90:00 - 91:00 4/TEC 2-72 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN .

CDR CMP LMP MCC—H 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 EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 91:00 - 92:00 4/TEC 2-73

MSC Form 1910 (Nov 08) FLIGHT PLANNING BRANCH 0 0 • 0 FLIGHT PL AN CDR OAP LMP MCC—H • I 92:00 e•-11L—i • 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 EDITION DATE TIME DAY/REY PAGE AS503/103 FINAL November 22,1968 92:00 - 93:00 4/TEC 2-74 MSC Form 1910 (Nov 69) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP CMP MCC—H 93: 00—

SLEEP PERIOD 93:30 - (5 HOURS) EAT PERIOD EAT PERIOD

MIR BIOMED Sw LEFT CMP/LMP CREW STATUS REPORT 94:00 —

94:30 - EAT PERIOD SLEEP PERIOD SLEEP PERIOD (5 HOURS) (7 HOURS)

95:00 ]

MISSION EDITION DATE TIME DAY/REV PAGE 4/TEC 2-75 AS503/103 FINAL November 22, 1968 93:00 - 95:00 MSC Farm 1910 (Nov BB) FLIGHT PLANNING BRANCH • 0 • 0 0 0 • 0 '0 FLIGHT PLAN CDR CMP thiP MCC—H 95:00_ • • I CDR CREW STATUS REPORT

95:15 -

SLEEP PERIOD PERIOD S SLEEP 95:30 — (5 (5 HOURS) F 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 DAY/REV PAGE AS503/103 FINAL November 22, 1968 95:00 - 96:00 4/TEC 2-76 MSC Farm 1918 (Nov 68) FLIGHT PLANNING BRANCH

FLIGHT PLAN

CDR CMP LMP 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 SLEEP PERIOD 96:30 — (5 HOURS) (5 HOURS)

96:45 —

97:00 :1 I

MISSION EDITION DATE TIME DAY/REV PAGE 2-77 AS503/103 FINAL November 22, 1968 96:00 - 97:00 5/TEC MSC Form 1910 (Nov E8) FLIGHT PLANNING BRANCH 0 0 0 • • • FLIGHT PLAN CDR C MP LMP MCC—H 97: 00—

97:30 -

SLEEP PERIOD SLEEP PERIOD 98:00_ (5 HOURS) (5 HOURS) F N

98:30 -

99:00 • •

MISSION EDITION DATE TIME DAY/REV PAGE 5/TEC 2-78 AS503/103 FINAL November 22, 1968 97:00 - 99:00 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PL AN

CDR CMP LMP MCC—H 99:00 — BIOMED Sw -, CENTER

99:15 -

99:30 — EAT PERIOD I EAT PERIOD EAT PERIOD

1=1

99:45 -

100:00

MISSION EDITION DATE TIME DAY/ REV PAGE AS503/103 FINAL November 22, 1968 99:00 - 100:00 5/TEC 2-79 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 0 0 ••• FLIGHT PLAN

CDR CMP LMP MCC—H 100:00 MNVR TO P52 ATT IMU REALIGN P52 CMP/LMP CREW STATUS OPTION 3 - REFSMMAT REPORT STAR ID STAR ANGLE DIFF TORQUE ANGLES: X 100:15

MNVR TO SIGHTING ATT TRN BIAS

LCISLUNAR NAVIGATION P231 100:30 1. STAR 02 LNH STAR L H 1 SET --

2. STAR 11 LFH STAR L H 1 SET 100:45 3. STAR 01 LNH STAR L H 1 SET

MNVR TO SIGHTING ATT 10 1 :00 •

MISSION EDITION DATE TIME DAY/REV PAGE 2-80 S503 103 FINAL November 22, 1968 100:00 - 101:00 5/TEC MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP IMP MCC—H 101:00 • •

101:15

TRN BIAS

CISLUNAR NAVIGATION P23 101:30 STAR 22 EFH STAR E H 2 SETS

• STAR 26 ENH STAR E H 101 :45 2 SETS

BIOMED Sw - RIGHT 102:00 a

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 101:00 - 102:00 5/TEC 2-81 MSC Form 1910 (Nov 00) FLIGHT PLANNING BRANCH 0 0 0 0 FLIGHT PL AN MCC—H CDR CMP LMP I 102:00 3 . STAR 31 ENH STARE H 2 SETS --

102:15

P27 UPDATE STATE VECTOR 102:30 TGT LOAD REFSMMAT VOICE UPDATE: MNVR TO P52 ATT RECORD MNVR PAD MNVR PAD IMU REALIGN P52 102:45 OPTION 3 - RESFMMAT STAR ID STAR ANGLE DI FF- TORQLTE ANGUE-S. .-- -- X

103:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 102:00 103:00 5/TEC 2-82 MSC Form 1919 (Nov ES) FLIGHT MCC BURN STATUS REPORT ' S X X tTIG BURN CHART X X ,BT V P or Y ATT SHUTDOWN gx RATES DEVIATION TIME RESIDUALS ----7TRIM _ X X X R MCC(ALL) 10°/SEC 10° B/T +1 SEC TRIM TO 0.2 fos TAKEOVER TAKEOVER X X X P 'XXX V gx V ;\) ....+ _. gY 1 coI.) 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 ,

CDR CMP LMP MCC —H 103:00 • • I

103:15 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 TRANS TO COUCH PIPA BIAS CK

SM RCS MON CK TEI+15 GDC ALIGN TO IMU 104:00 1CT 5 0.--- NOMINALLY ZERO

, MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 103:00 - 104:00 5/TEC 2-83 MSC Form 1210 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC-11 104:00 -- • I V66 TRANS CSM STATE MCC 5 BURN STATUS REPORT VECTOR TO LM SLOT SM RCS MON CK INITIATE BAT CHARGE

UNSTOW TV CAMERA

104:15 —

TV

104:30 — F EAT PERIOD EAT PERIOD EAT PERIOD N .l- STOW TV CAMERA

104:45 —

CDR CREW STf TUS REPORT 105:00 —1

MISSION EDITION DATE TIME DAY/REV PAGE FINAL November AS503/103 22 1968 104:00 - 105:11 1111/111111111/111111 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 0 0 0 FLIGHT PLAN LMP MCC—H CDR crow 6 105:00-- • • LiOH CANISTER CHANGE (CARTRIDGE NO. 12 FROM B6 INTO CANISTER 13) BIOMED Sw - CENTER TRANS TO LH COUCH MNVR TO SIGHTING ATT

105:15 - TRN BIAS CISLUNAR NAVIGATION P23 1. STAR 22 EFH STAR E H 2 SETS M S SLEEP PERIOD 105:30 — F N (7 HOURS)

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

3 . STAR 31 ENH STAR E H 2 SETS • 106:00--

PAGE MISSION EDITION DATE TIME DAY/REV AS503/103 FINAL November 22, 1968 105:00 - 106:00 5/TEC 2-85

MSC Form 1610 (Nov 68) FLIGHT PLANNING N FLIGHT PLAN

CDR CMP LMP MCC —H 106:00 • • S

MNVR TO SIGHTING ATT

TRN BIAS 106:15 1. STAR 02 LNH STAR L H 1 SET

2. STAR 11 LEH STAR L H 106:30 S SLEEP PERIOD F (7 HOURS) 1 SET N

3. STAR 01 LNH STAR L H 1 SET

106:45 RETURN TO EARTH P37

107:00-1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 106:00 - 107:00 5/TEC 2-86 MSC Form i9:0 (Nov 68) FLIGHT PLANNI 0 0 0 0 • 41 • 0 I . FLIGHT PLAN LIMP MCC—H CDR • 107:00

107:15

S 107:30 F SLEEP PERIOD N (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 TIME DAY/REV PAGE AS503/103 FINAL. November 22,1968 107:00 - 108:00 5/TEC 2-87 MSC Form 191O (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC—H 108:00 -- • • • CISLUNAR NAVIGATION P231 BIOMED Sw - RIGHT 1. STAR 22 EFH STAR E H 1 SET

108:15 -

2. STAR 26 ENH STAR E 2 SETS -- 1 108: 30— SLEEP PERIOD (7 HOURS) -I

3. STAR 31 ENH STAR E H 2 SETS 108:45 MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1°/SEC P&Y FREE RETURN TO EARTH P37 REESTABLISH PTC AT +15° IN P OR Y AND RECORD GET

109:00 :1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 108:00 - 109:00 5/TEC 2-88 MSC Form 1910 (Nov 08) FLIGHT PLANNING BRANCH 9 0 0 • FLIGHT PLAN

CDR CMP LMP MCC—H • 109:00 •

109:30

H S SLEEP PERIOD 1 10:0 0 F N (7 HOURS)

110: 3 0

111:00 • •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 109:00 - 111:00 5/TEC 2-89 MSC FLIrm 1910 (Nov 6$) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC— H 111:00

111:30 SLEEP PERIOD EAT PERIOD I EAT PERIOD (7 HOURS)

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

112:30 EAT PERIOD SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

113:00 -I

MISSION EDITION DATE TIME DAY/ Inv PAGE AS503/103 FINAL November 22, 196e 111:00 - 113:00 L 5/TEC 2-90 MSC Form 1910 (Nov 58) FLIGHT PLANNING BRANCH 0 0 0 • • 4• FLIGHT PLAN

CDR CMP LMP MCC-H 113:00 f

CDR CREW STATUS REPORT

113:30 -

.M1

S 114:00 — F SLEEP PERIOD SLEEP PERIOD N (7 HOURS) (7 HOURS)

114:30

.=1

MNVR TO P52 ATT 115:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 113:00 - 115:00 5/TEC 2-91 MSC Form 19:0 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP L PAP MCC—H 115:00 4 IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF TORQUE ANGLES: X 115:15 Y

MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1 °/SEC 115:30 SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

115:45

116:00 i

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 115:00 - 116:00 5/TEC 2-92 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0

0 0 • • FLIGHT PL AN CDR CMP LMP MCC-H 116:00

116:30

117:00 SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

117:30

118:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 116:00 - 118:00 5/TEC 2-93 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP L MP MCC ..-14 S 118:00 — •

118:30 - EAT PERIOD SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

LiOH CANISTER CHANGE M (CARTRIDGE NO. 13 FROM S B6 INTO CANISTER A) 119:00 — F N BIOMED S - CENTER

119:30 — EAT PERIOD EAT PERIOD

1

MNVR TO SIGHTING ATT TRN BIAS 120:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 118:00 - 120:00 5/TEC 2-94

MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 • 0 0 FLIGHT PLAN CMP LMP MCC—H CDR • 120:00 - • • CISLUNAR NAVIGATION P23 CMP/LMP CREW STATUS REPORT . STAR 22 EFH STARE H 1 SET -

. STAR 26 ENH 120:15 - STAR E H 1 SET —

. STAR 31 ENH STAR E H 1 SE7- - —

120:30

120:45 - P27 UPDATE: STATE VECTOR TOT LOAD RECORD MNVR PAD VOICE UPDATE: MNVR PAD 121:00 --

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 120:00 - 121:00 6/TEC 2-95 MSC Form 1919 (Nov 98) FLIGHT PLANNING BRANCH MCC'S BURN STATUS REPORT • X X _ATIG BURN CHART X X • BT P or V ATT SHUTDOWN V gx RATES DEVIATION TIME RESIDUALS TRIM. X X X R MCC(ALL) 10°/SEC 10° B/T +1 SEC TRIM TO 0.2 fns TAKEOVER TAKEOVER X X X P X X X Y V gx V gY V c) 9.2 AV c X X X FUEL X X X Ox X X X UNBALANCE REMARKS:

• 0 0 • '

FLIGHT PL AN CDR CMP LMF MCC—H 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 EMS TEST TRANS TO COUCH PIPA BIAS CK

GDC ALIGN SM RCS MON CK TEI f 33 HRS ❑ MCC 6 V=NOMINALLY ZERO 122:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 121:00 - 122:00 6/TEC 2-96 MSG Form 1810 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC—H 122:00 I V66 TRANS CSM STATE SM RCS MON CK MCC BURN STATUS REPORT VECTOR TO LM SLOT 6 INITIATE BAT CHARGE

STONED Sw - RIGHT

122:15

122:30 MNVR TO SIGHTING ATT

TRN BIAS 1CISLUNAR NAVIGATION P231 1. STAR 02 LNH STAR L H 2 SETS 122:45

I 2. STAR 01 LNH STAR L H 123:00 1 SET

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 122:00 - 123:00 6/TEC 2-97 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 0

FLIGHT PLAN

CDR CMP OAP MCC—H 123:00 • • RETURN TO EARTH P37

MNVR TO SIGHTING ATT

123:30

123:30 F N TRN BIAS 1 [CISLUNAR NAVIGATION P23 1. STAR 22 EFH STAR E H 123:45 2 SETS —

2. STAR 26 ENH STAR E H 1 SET 124:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 123:00 - 124:00 6/TEC 2-98 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP 1MP MCC—H 124:00 —,

STAR 31 ENH STAR E H 2 SETS —

124:15 -

MNVR TO PTC ATT 124:30 P 029 Y 315 RETURN TO EARTH P37

ROLL 0.17 EC

124:45 -

125:00-1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 124:00 - 125:00 6/TEC 2-99 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 • 0 0 • 0 • • FLIGHT PLAN CDR CMP LMP MCC—H 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 127:00 -- 6 4

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 125:00 - 127:00 6/TEC 2-100 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 127:00 — LiOH CANISTER CHANGE (CARTRIDGE NO. 14 FROM B6 INTO CANISTER B)

127:30

11.

BIOMED Sw - RIGHT

UNSTOW TV CAMERA 128:00 — SLEEP PERIOD (7 HOURS) TV .m1

STOW TV CAMERA

128:30 —

i

129:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 127:00 - 129:00 6/TEC 2-101 MSC Form 1610 (Nov 68) FLIGHT PLANNING BRANCH 0 0 0 FLIGHT PLAN CMP LMP MCC —H CDR • I 129:00 — • •

129:15 -

M S 129:30 — F SLEEP PERIOD N (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

TRN BIAS MNVR TO SIGHTING ATT 130:00-- • •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 129:00 - 130:00 6/TEC 2-102

MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 130:00 — • CISLUNAR NAVIGATION P23 '

STAR 02 LNH H STAR_ — 2 SETS

130:15 -

S 130:30 — F SLEEP PERIOD N (7 HOURS) MNVR TO SIGHTING ATT

130:45 — TRN BIAS

. STAR 22 EFH STAR E H 2 SETS

131:00 S

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 130:00 - 131:00 6/TEC 2-103 MSC Forin 1910 (NoV $8) FLIGHT PLANNING BRANCH • 0 0 0 0

FLIGHT PLAN

CMP LMP MCC-H CDR 6 131 :00 BIOMES Sw - CENTER

2. STAR 26 ENH STAR E H 131 :15 2 SETS

S 131 :30 F SLEEP PERIOD 3. STAR 31 ENH N (7 HOURS) STARE H 2 SETS --

131:45

MNVR TO PTC ATT P 029 Y 315 P Y RETURN TO EARTH P37 ROLL 0.1°/SEC 132:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 131:00 - 132:00 6/TEC 2-104 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 132:00 EI -15 HRS . P27 UPDATE: STATE VECTOR STATE VECTOR GO/NO GO GO/NO GO RECORD BLOCK DATA VOICE FOR EI -2 HOURS UPDATE: BLOCK DATA 13230 FOR EI -2 HOURS MCC

133:00 SLEEP PERIOD (7 HOURS)

133:30 EAT PERIOD I EAT PERIOD

CMP/LMP CREW STATUS REPORT BIOMED Sw - _ LEFT

1 3 4:00 -1

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 132:00 - 134:00 6/TEC 2-10 5 11SC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 e0 • • • 4; FLIGHT PL AN

CDR CMP LMP MCC- H 134:00

134:15

134:30 EAT PERIOD SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

134:45

135:00 •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 134:00 - 135:00 6/TEC 2-106 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PLAN

CDR CMP LMP MCC—H 135:00 • BEGIN CABIN COLD SOAK CDR CREW STATUS REPORT

135:15 -

MNVR TO P52 ATT SLEEP PERIOD SLEEP PERIOD 1 IMU REALIGN P52 (7 HOURS) (7 HOURS) 135:30 — OPTION 3 - REFSMMAT STAR ID , STAR ANGLE DIFF TORQUE ANGLES: X

135:45

REESTABLISH PTC P 029 Y 315 P Y ROLL 0.1'/SEC 136:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 135:00 - 136:00 6/TEC 2-107 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH 0 •

0

FLIGHT PLAN CDR CMP LMP MCC—H 136:00 — s.

136:30 -

SLEEP PERIOD SLEEP PERIOD M (7 HOURS) (7 HOURS) 137:00 — S F

137:30 -

•

138:00 —

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22 o 1968136:00 - 138:00 6/TEC 2-108 MSC Finn 1910 (Nov 68) FLIGHT PLANNING BRANCH

FLIGHT PLAN

CDR CMP LMP MCC—H 138:00 6

138:15

SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)

138:30

138:45

139:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 196E 138:00 - 139:00 6/TEC 2-109 MSC Form 1910 (Nov 66) FLIGHT PLANNING BRANCH 0 0 • • FLIGHT PLAN CMP LMP MCC—H CDR 6 139:00 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 - SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS) 139:30 TORQUE ANGLES: X

REESTABLISH PTC P 029 Y 315 139:45 P Y ROLL 0.1°/SEC

• 140:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 196S 139:00 - 140:00 6/TEC 2-110 MSC Form :9i (Nay 68) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP OAP MCC— H 140:0

140:15

EAT PERIOD SLEEP PERIOD SLEEP PERIOD (7 HOURS) 140:30 (7 HOURS)

140:45

141 :00

MISSION EDITION DAT E TIME DAY/REV - PAGE AS503/103 FINAL November 22,1968 140:00 - 141;00 2-111 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH

0 • 0 j ip 0 0 • FLIGHT PLAN

CDR CMP LMP MCC—H 141:00 I MNVR TO SIGHTING ATT LOSS OF COMM CONTINGENCY TRN BIAS BIOMED Sw - RIGHT' [CISLUNAR NAVIGATION P23

1. STAR 22 EFH STAR E H 1 SET 141:15 2, STAR 26 ENH STAR E H 1 SET— STAR 31 ENH STAR E H 1 SET — 141:30

EAT PERIOD I EAT PERIOD - 141;45

142:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 141:00 - 142:00 2-112 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH FLIGHT PL AN CDR CMP LMP MCC-H 142:00 4

EAT PERIOD EAT PERIOD

142:15

142:3 LOSS OF COMM CONTINGENCY

TRN BIAS ISLUNAR NAVIGATION P231

1. STAR 22 EFH STAR E H 142:45 1 SET

2. STAR 26 ENH I STAR E-- H 1 SET

143:00-1 • •

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22,1968 142:00 - 143:00 2-113

MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH • 0 0 • FLIGHT PL AN

CDR CAW OAP MCC- Ii 143:00 • ar

P27 UPDATE: STATE VECTOR (LM & CSM SLOTS) El-3.5 HRS REFSMMAT RECORD MNVR AND ENTRY VOICE PAD 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— -- EI-3 HRS X EPS CK SPS CK SM/CM RCS CK C&W CK CMC SELF CK DSKY COND LT TEST 144:00 •

MISSION EDITION DATE TIME DAY/REV 2 PAGE AS503/103 FINAL November 22, 1968 143:00 - 144:00 6/TEC -114 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH

BURN STATUS REPORT MCC'S X --..+. ■ X ATIG BURN CHART 1 X X • • T P or Y ATT SHUTDOWN _ g x , • I RATES DEVIATION TIME RESIDUALS . W___1174 X X X IR MCC(ALL) 10°/SEC 10° BIT +1 SEC TRIM TO 0.2 fps TAKEOVER TAKEOVER X X I P X X X 1 Y gx !V i V gy F-1 IVgz AV C X X i ;FUEL X X ; OX X X X , ;UNBALANCE 'REMARKS:

0 0 ill I + 410 0 FLIGHT PLAN

CDR CMP LMP MCC-H 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 EI-2 HRS MCC 7 AV=NOMINALLY ZERO MCC BURN STATUS REPORT V66 TRANS CSM STATE VECTOR TO LM SLOT

.145:00 •

MISSION EDITION DATE allIMIE31.11. DAY/REV =MI AS503 103 FINAL November 22, 196 144:00 - 145:00 7/TEC 2-115 MSC Form 1910 (Nov 08) FLIGHT PLANNING BRANCH FLIGHT PLAN CDR CMP LMP MCC-H 145: 00 — LOSS OF COMM CONTINGENCY BIOMED Sw - LEFT CISLUNAR NAVIGATION P23 1. STAR 33 ENH STARE H 1 SET -- -- MNVR TO ENTRY ATT CCU STAR CK SXT STAR CK

IMU REALIGN P52 OPTION 3 - REFSMMAT EI-1.5 HR DRIFT TEST AND GYRO PIPA BIAS STAR ID , -- STAR ANGLE DIFF CK

TORQUE ANGLES: X 145:30 — Y

GDC ALIGN TO IMU

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

E I -1 HR EMS CK

FINAL GDC DRIFT CK 146:00 —1

PAGE MISSION EDITION DATE TIME r DAY/REV November 22, 196E 145:00 - 146:00 7/TEC 2-116 AS503/103_ FINAL MSC form 1310 (Nov 68) FLIGHT PLANNING BRANCH • 0 • 4I■ 0 FLIGHT PL AN

CDR CMP LMP MCC—H 146:00 • I TERM CM RCS PREHEAT PYRO BAT CK P27 UPDATE: STATE SET DET TO EI VECTOR EMS INITIALIZATION VOICE RSI ALIGN TO GDC RECORD ENTRY PAD & RCVY UPDATE: CM RCS CK INFO ENTRY PAD & RCVY INFO

EI-30 MIN ENTRY BATS - ON

SEPARATION CK LIST SEPARATION CK LIST SEPARATION CK LIST

146:30 MNVR TO CM/SM SEP ATT P61 ENTRY PREP GO FOR PYRO ARM GO FOR PYRO ARM EI-15 MIN [CM/SM SEP MNVR TO ENTRY ATT P62 ENTRY ATTITUDE

P63 ENTRY INITIATE 146:50 [ET = 4QOK1 P64 ENTRY POST .05G

147:00

MISSION EDITION DATE TIME DAY/REV PAGE AS503/103 FINAL November 22, 1968 146:00 - 147:00 7/TEC 2-117 MSC Form 1910 (Nov 98) FLIGHT PLANNING BRANCH

FLIGHT PLAN CDR CMP LMP MCC-H 147 : 00 — • • • •

EARTH LANDING PHASE

LSPLASHDOWN

147:30 —

148:00 — •

MISSION EDITION DATE TIME DAY/REV PAGE SE03/103 FINAL November 22, 1968 147:00 - 148:00 7/TEC 2-118 MSC Form 1910 (Nov 60) FLIGHT PLANNING BRANCH 0 0 • •