APOLLO 8 FLIGHT PLAN - . – The Public's Library and ... · Flight Plan Notes 1-4 ... Abort...
Transcript of APOLLO 8 FLIGHT PLAN - . – The Public's Library and ... · Flight Plan Notes 1-4 ... Abort...
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
Approved by: ,,, W. J. North
Chief, Flight Crew Support Division
et,
APOLLO AS503/CSM 103
FINAL FLIGHT PLAN
November 22, 1968
Submitted by: Cr a T. A. Guillory Flight Planning Branch
,
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
Abbreviations
Section I - General
ii
iii
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
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
DAP D/B DEDA DEGS DEPL DET DIFF DK DOI
ACCEL
Accelerometer ACT
Activation ACQ
Acquisition AEA
Abort Electronics Assembly AGS
Abort Guidance Sybsystem Ali
Ampere Hours ALIGN
Alignment ALT
Altitude AMP or amp Ampere AMPL Amplifier ANG Antigua Ant Antenna AOS Acquisition of Signal AOT
Alignment Optical Telescope APS
Ascent Propulsion Subsystem ARS
Atmosphere Revitalization H. ASC
Ascension AS CT
Ascent ATT
Attitude AUX
Auxiliary AZ
Azimuth
BAT
Battery BDA
Bermuda BP
Barber Pole BT
Burn time Bio Bio-Medical Data on Voice Downlink
B iW
Black & white BU
Backup BRKT
Bracket
CAL
Pt. Arquillo, California CAL
Calibration Angle CAM
Camera CB
Circuit Breaker
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
Digital Auto Pilot Deadband Data Entry and Display Assembly Degrees Depletion Determination or Digital Event Timer Difference Docked Descent Orbit Insertion
ABBREVIATIONS (Cont'd)
Descent Propulsion Subsystem Data Storage Equipment Display and Key Board Detailed Test Objective Digital Uplink Assembly Down
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
F Stop Fuel Cell Flight Director Attitude Indicator Flight Frequency Modulated Field of View Feet per second Flight Qualification Feet Full Throttle Position
Grand Bahama Gyro Display Coupler Goldstone, California
GET
Ground Elapsed Time GETI
Ground Elapsed Time of Ignition GLY
Glycol GMT
Greenwich Mean Time G&N
Guidance and Navigation GNCS
Guidance Navigation Control System GWM
Guam GYM
Guaymas, Mexico
HA
Apogee Altitude HAW
Hawaii HBR
High Bit Rate (TLM) HD
Highly Desirable HGA
High Gain Antenna HI
High Hp Perigee Altitude HSK
Honeysuckle (Canberra, Australia) HTR
Heater HTV
USNS Huntsville
ID
Identification IGN
Ignition IAN
Inertial Measurement Unit INIT
Initialization INT
Intervalometer IP
Initial Point IU
Instrumentation Unit I VT
Intravehicular Transfer
JETT
Jettison
kwh
Kilowatt Hour
LAT Latitude LBR Low Bit Rate (TLM) LBS or lbs Pounds
DP S DSE DSKY DIO DUA DWN
E ECS EPH EI ELDMK EMS ENU EPO EPS EQUIP EST EVAP EVT EXT
FC FDAI FLT FM FOV fps FQ FT or ft FTP
GBI GDC GDS
0 0 • LCG LDG LDMK LEB LFH
ABBREVIATIONS (Cont'd)
Measurement DSNS Mercury Mission Event Timer Minimum Impulse Minimum
Liquid Cooled Garment Landing Landmark Lower Equipment Bay Lunar Far Horizon
MEAS MER MET M/I MIN
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)
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
Umbilical Undock United States Pass
Very High Frequency Valve Verb xx
Without With Respect to USNS Watertown
Transfer Transmit or Transmitter Transponder
AV
Velocity Change (Differential) AV C
Velocity Change at Engine Cutoff AR
Position Change (Differential)
8-balls Flight Director Attitude Indicator (FDAI) LBS or lbs 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 POL FILTER 1/4 - Polarization filter, Shutter Speed 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
TEMP TERM TEX T &D TGT TIC TLC TLI TLM TPF TPI TPM T/R TRANS TV TVC TWR
UMB UNDK US
VHF VLV Vxx
W / 0 WRT WTN
XFER XMIT XPONDER
Yaw
LUNAR TERMINATOR
SPACECRAFT SUNSET
ESFN LOS
DARKNESS
SPACECRAFT SUNRISE
LUNAR TERMINATOR
WINDOW (HEADS UP)
S-DAND EGA
OPTICS LUNAR SURFACE
POINT
MSPN AOS
S
N
EARTH
viii
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 MCCl'
a series of star/earth landmark sightings is scheduled at which
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
410
•
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
4 is scheduled. The OMP and LMP sleep period
(62:00 GET) is scheduled between MCC4 and LOI1 .
At 69:07 GET, the LCII maneuver places the S/C into a 60 x 170-nm lunar
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
5 at TEI 15 hours (104:00 GET), followed by
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
1 -2 minutes to end of tape
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.
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
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
x
X
X
x X . X
X X X
X X X
H i
.
IR
P
Y
X X X ; X X X ; BT
+ •
+
, .8VC I
VI
X
X
X
X
X
X
X
X
X
X , X ,.X
X X X
X X 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 (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) P SEP XXX (DEG) Y SEP XXX (DEG)
PREDICTED SPACECRAFT IMU GIMBAL ANGLES AT COMPLETION OF S-IVB MNVR TO CSM/S-IVB SEP ATTITUDE
P27 UPDATE
PURP V V
GET • • IS
304 0
02
03
04
05
06
07
10
II
12
13
14
15
1 6
17
20
2I
22
23
24
INDEX INDEX INDEX
F
'
1--
N34 HRS
MIN
NAV CHECK SEC
X X X
X X XX
X X
X X X
X X•X X
X•X • I N43 LAT
LONG
ALT
0 •
0
0 ,
_• , 1 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 •
NDRTH L SOUTH SET STARS
R ALIGN 0 0
0 P ALIGN 0
Y ALIGN I+
+
+
0
0
0
0
0
ULAGE
X X
X X
HX X
X
X
X
U
• •
PUR;'051::
P.S'OP/GUk:)
; . J 47
PTRhA " 8
YTRI: A
HRS GET
WN N33
SEC
nvx NE-1
LIVy
R
nVZ
WT
N4-3- 1
•
P •
:]VT
i3T
.]VC HORIZON/WINDOW X X X
X
•
X XX X
•
X X X
X X
X X XI
SXTS
0 SFT
0 .SRN
BSS
SPA • , S X P
OT H ER 0 LAT N61
LONG 11/_----,L--
RTGO EMS
VIO
• • • I GET .05G •
1-12
R P Y
H A
H P
AVT
BT
AVC
SXTS
SFT
TRN
BSS
SPA
XXX (DEG) XXX (DEG) XXX (DEG)
XXXX.X (nm)
XXXX.X (nm)
XXXX.X
X:XX (MIN:SEC)
XXXX.X (fps)
XX (OCTAL)
XXX.X (DEG)
XX.X (DEG)
XXX (OCTAL)
XX.X (DEG)
MANEUVER PAD
PURPOSE XXXXXX
PROP/GUID
TYPE OF MNVR TO BE PERFORMED
PROPULSION SYSTEM (SPS/RCS)/ GUIDANCE (SCS/G&N)
WT
P TRIM
Y TRIM
XXXXX (lbs)
X.XX (DEG)
X.XX (DEG)
PREMANEUVER VEHICLE WEIGHT
SPS PITCH GIMBAL OFFSET TO PLACE THRUST
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
IMU GIMBAL ANGLES OF MANEUVER ATTITUDE
PREDICTED APOGEE ALTITUDE AFTER MANEUVER
PREDICTED PERIGEE ALTITUDE AFTER MANEUVER
TOTAL VELOCITY OF MANEUVER
MANEUVER DURATION
PREMANEUVER AV SETTING IN EMS AV COUNTER
SEXTANT STAR FOR MANEUVER ATTITUDE CK
SEXTANT SHAFT SETTING FOR MANEUVER ATTITUDE CK
SEXTANT TRUNNION SETTING FOR MANEUVER ATTITUDE CK
BORESIGHT STAR FOR MANEUVER ATTITUDE CK USING THE COAS
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
ULLAGE
HORIZON WINDOW
RANGE TO GO FOR EMS INITIALIZATION
INERTIAL VELOCITY AT .05G FOR EMS INITIALIZATION
TIME OF .05G
STARS FOR TELESCOPE FOR BACKUP GDC ALIGN
ATTITUDE TO BE SET IN ATTITUDE SET TW FOR BACKUP GDC ALIGN
NO. OF SM RCS JETS USED AND LENGTH OF TIME OF ULLAGE
WINDOW MARKING AT WHICH HORIZON IS PLACED AT A SPECIFIED TIG (ATT CK)
RTGO XXXX.X
VIO XXXXXX (fps)
GET(.05G) XX:XX:XX
NORTH & SOUTH SET STARS
R, P, Y ( ALIGN)
ENTRY
AREA
X
X
X
X
X
X
X
X
R .05G
P .05G
Y .05G
X
GET HOR
P CK X X
0 LAT N6 I
LONG
X X MAX G
, 0 0
V400K N60
T4OOK
4- 1
RTGO EMS
VIO
• RRT
X X • RET. 05G* • + 0 ' +i 0
0
0
DL MAX -
DL M IN*N69
VL MAX*
I VL M I N*
• •
X . X X Do •
X X • RET VCIRC •
X X • RETB BO 4 . X , X
• RETEBO •
X X • RETDRO
0
X X X X
;0 0
SX TS
SFT
TRN
X X
X X
X X
X
• _
•
BSS
SPA
SXP X
X X X X LIFT VECTOR
• • • • x x
• X X
xIxIx x xxix
0 0
+ +
+ 0 0
+ 0 0 .
X X X
X X
x x: X X
X :X . X X
!O
X X X
X X
X X X
X X X X.
• •
• •
•
•
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
RRT
RET .05G
D L MAX
D MIN
V MAX
V MIN
XX:XX:XX TIME OF ENTRY ATTITUDE (HRS:MIN:SEC). HORIZ CHECK AT EI -17 MIN.
XXX(DEG) PITCH ATTITUDE FOR HORIZON CHECK AT EI -17 MIN
±XX.XX(DEG) LATITUDE OF TARGET POINT
±XXX.XX(DEG) LONGITUDE OF TARGET POINT
XX.X (G's) PREDICTED MAXIMUM REENTRY ACCELERATION
XXXXX (fps) INERTIAL VELOCITY AT ENTRY INTERFACE
X.XX(DEG) INERTIAL FLIGHT PATH ANGLE AT ENTRY INTERFACE
+XXXX.X(nn) RANGE TO GO FROM .05G TO TARGET FOR EMS INITIALIZATION
+XXXXX.(fps) INERTIAL VELOCITY AT .05G FOR EMS INITIALIZATION
XX:XX:XX (HRS:MIN:SEC) REENTRY REFERENCE TIME BASED
ON GET OF PREDICTED 400K (DET START)
TIME OF .05G FROM 400K (RRT)
MAXIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC)
MINIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC)
MAXIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC)
XXXXX (fps) MINIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC)
GET (H0R CK)
P (HOR CK)
LAT
LONG
MAX G
V400K
Y400K
RTGO
VIO
XX:XX (MIN:SEC)
X.XX (G's)
X.XX (G's)
XXXXX (fps)
1-16
ENTRY PAD (cont'd)
DO X.XX (G's) PLANNED DRAG LEVEL DURING CONSTANT G
RET V CIRC XX:XX TIME FROM EI THAT S/C VELOCITY (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
1-18
REMARKS REV 3/4 .
GET (hrs:min:sec)
LOS
SR
PM
AOS
SS
MAP UPDATE
REV 1/2
GET (hrs:min:sec)
LOS
PM AOS
SS
LOS
SR
PM
AOS
SS
REMARKS
REV 2/3
GET (hrs:min:sec)
LOS
SR
PM
AOS
SS
REMARKS
REV 7/8
GET (hrs:min:sec) LOS
REMARKS
PM • .
. AOS -
SS . .
• .
- .
REV 8/9
GET (hrs:min:sec)
LOS .
• SR .
PM '
AOS
- SS .
• .
:
:
- .
REMARKS
REV 9/10
GET (hrs:min:sec)
LOS
REMARKS
• — . SR -
PM ' AOS .
' SS
REV 10 GET (hrs:min:sec)
LOS - • SR . . • ADS •
SS '
REMARKS
• MAP UPDATE
1-19
REV 4/5
GET (hrs:min:sec)
LOS ' . SR •
PM
AOS
SS •
-
• .
• ' .
•
REMARKS
REV 5/6
GET (hrs:min:sec)
LOS .
SR
• PM .
AOS :
SS
.
.
. -
REMARKS
REV 6/7
GET (hrs:min:sec)
LOS .
SR • .
• PM .
• AOS .
• SS .
• .
• .
* REMARKS
MAP UPDATE
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
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
00:00 CDR CMP
• LMP
• MCC-H
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
T CDC ALIGN TO IMU INGRESS LEB EPS PERIODIC MONITOR
C 0 2 MAIN'REG CK ECS MONITOR CK
00:30 MOUNT & INITIALIZE SPS PERIODIC MONITOR ORDEAL PUGS TEST
T INSTALL COAS JETTISON OPTICS COVER ECS REDUNDANT COMP CK
A COAS HORIZON CK RECORD AAZ CORRECTION FC PURGE OK VOICE N UPDATE:
AAZ CORREC- TION
00:45
1- OPTICS CK IMU REALIGN P52
CR OPTION 3 - REFSMMAT BIOMED Sw - CENTER ] 0 STAR ID J- —Tc'Erit'd)
01:00 •
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 00:00 - 01:00 1 /LPO 2-1 MSC Form 1910 (0T) Oct 68) FLIGHT PLANNING BRANCH
0 0 0 0
• • 0 41 FLIGHT PLAN
01:00
01:15
01:30
01:45
02:00
S
Y
CDR
SCS ATT REFERENCE COMPARISON CK
CMP
STAR ANGLE RIFF
TORQUE ANGLES:. X __. Y
LMP •
BACKUP COMM CK
BIOMED Sw - RIGHT
•
GIVE GO FOR COMM CK
VOICE UPDATE: BLOCK DATA
VOICE UPDATE: TLI PAD
P27 UPDATE: STATE VECTORS
REPORT: GYRO TORQUE ANGLES
RECORD ABORT BLOCK PAD (TLI +90 MIN AND TLI +4 HOUR)
RECORD TLI PAD
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
0
X X ATIG
X X BT
V gx TRIM
X X X R
X X X P
X X X Y Vi
h AV c
X X X
FUEL
X X X
Ox
I XXX
UNBALANCE
REMARKS:
TLI BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
TLI 10°/SEC SHUTDOWN
+45° SHUTDOWN
B/T+6 SEC & Vi=PAD VALVE NO TRIM
TLI PREMATURE SHUTDOWN
ha >60,000 nm LUNAR ORBIT OR FLYBY (DEPENDING ON AV REQD: TWO PHASING MANEUVERS TO SEMI-SYNCHRONOUS ORBIT. DIRECT ENTRY
ha >22,000 nm
ha >41,000 nm HIGH ALTITUDE ORBITS FOLLOWED BY DEBOOST TO 400 nm APOGEE
h a 100 - 41,000 nm EITHER HI ALTITUDE (41,000 ha) OR LOW ALT, DEPENDING ON LANDMARKS
BIOMED Sw - LEFT
FLT RCDR - RECORD
IGETI = 2:50:31
FLT RCDR - OFF
•
0 0 • 0 • CDR
TLI PREP EMS AV TEST
GO/NO-GO FOR PYRO ARM GO/NO-GO FOR TLI
FLIGHT PLAN CMP
•
TLI PREP TLI PREP TRANS TO COUCH
LMP •
MCC-H •
GO/NO-GO
GDC ALIGN AND DRIFT CK
TB-6
P47 BURN ATT CK
SECO S-IVB INERTIAL SECO +20 SEC S-IVB TO LH 2 ORB RATE,HEADS DOWN
MISSION EDITION DATE TIME DAY/REV MOE
AS503/103 FINAL November 22,1968 02:00 - 03:00 1/LPO 2-3
MSC Form 1910 (0T) (Oct 68) FLIGHT PLANNING BRANCH
FLIGHT PLAN 03:00
03:15
03:30
03:45
04:J
CDR
TLI BURN STATUS REPORT
S-IVB MNVR TO SEP ATT
GO/NO-GO FOR 90-MIN ABORT
TRANSPOSITION FROM S-IVB +X FOR 1 fps, COAST FOR 1 MIN, -X FOR 0.5 fps, PITCH UP 4°/SEC
FLY FORMATION
MNVR TO LOCAL VERTICAL -X RADIALLY UPWARD 1,5 fps
CMP •
RECORD GET SEP MNVR INIT
TRANS CSM STATE VECTOR TO LM SLOT
UNSTOW PHOTO EQUIP B3 16mm DAC
18mm LENS RT ANG MIRROR 16mm C-EX MAG PWR CABLE 70mm CAM 80mm LENS 70mm C-MAG
LMP
S-BAND XPONDER - SEC FLT RCDR - RECORD
FLT RCDR - OFF
NONESS BUS - OFF
PHOTOGRAPH S-IVB 16/18/C-EX, 1/250, fll, 6 fps (1 MAG) 2/80/C, 1/250, SPOT (10 EXP)
a
MCC-H
VOICE UPDATE: GET OF SEP MNVR INIT
GO/NO-GO
COMM TEST
MODE: 4.2
•
R13 SPOTMETER
DOFF & STOW PGA
TRANS CSM STATE VECTOR TO LM SLOT
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
CMP fi
LMP •
MCC—H
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF
REPORT PERSONAL RADIATION DOSIMETER READINGS
TORQUE ANGLES: X Y
rCISLUNAR 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
3. STAR 16 EFH STAR E H 2 SETS - 3 MARKS EACH
CDR 04:00
04:15 _
GDC ALIGN TO IMU
04:45 —
05:00 -- •
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
CDR
DOFF & STOW PGA
MNVR TO PTC ATT P 331 Y 331 P Y roll 0.1°/SEC
F
FLIGHT PLAN
05 :00 — CMP
GROUND TRACK DET P21
LMP •
RECORD BLOCK DATA (TLI +4 HRS & TLI +11 HRS)
MCC—H 6
VOICE UPDATE: BLOCK DATA
05:15 -
05 :30 —
BIOMED Sw - CENTER
DOFF & STOW PGA
05:45 -
KEY V64 S-BAND HIGH GAIN ANT CHECKOUT
COMM TEST MODES:
4.2 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) • CDR LMP MCC-H
FLIGHT PLAN CMP
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
FLIGHT PLANNING BRANCH MSC Form 1
FLIGHT PLAN
CDR •
CMP LMP MCC—H
PERFORM COMM TESTS MODES: 4.3
6.3 5.2 8.1
07:00
07:15 —
LiOH CANISTER CHANGE (CARTRIDGE NO. 3 FROM A3 INTO CANISTER A)
07:30
OPEN COOLANT CONTROL ATTENUATION PANEL EVAP WATER CONT SEC VLV - OFF
CLOSE COOLANT CONTROL ATTENUATION PANEL
07:45 —
I
08:00
WASTE STOWAGE VENT -CLOSED BAT VENT VLV - OPEN (UNTIL SERVICE METER = 0) BAT VENT VLV - CLOSED •
P27 UPDATE: STATE VECTOR TGT LOAD
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
BURN STATUS REPORT
• ; ATIG
• ST V gx
X x X x
1 1
.TRIM X X X
X X X
X X X
R
P
Y .V
gx V
• _ gY Vgz
AV c Co
0 0 0 0 MCC'S
BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
MCC(ALL) 10°/SEC TAKEOVER
10 0 TAKEOVER
B/T +1 SEC TRIM TO 0.2 fps
X X X FUEL X X X Ox X X X UNBALANCE
'REMARKS:
V47 TRANS LM STATE VECTOR TO CSM SLOT
PIPA BIAS CK
08:30 EXT AV P30 SPS/RCS THRUST P40/P41 MNVR TO BURN ATT
BIOMED Sw - RIGHT
CMP
IMU REALIGN P52 OPTION 3 - REFSMMAT AND DRIFT CK STAR ID STAR ANGLE DIFF
TORQUE ANGLES-- -- X Y
08:00 CDR •
MNVR TO P52 ATT
LMP •
RECORD MNVR PAD
MCC—H •
VOICE UPDATE: MNVR PAD
08:15
SXT STAR CK
TRANS TO COUCH
08:45
:1 TLI +6 HRS 09:00
EMS AV TEST
GDC ALIGN
MCC, AV--NOtilINALLY ZERO
FLIGHT PLAN
MISSION EDITION DATE TIME DAY/REV PAGE
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 • 09:00
CDR •
V66 TRANS CSM STATE VECTOR TO LM SLOT
MCC 1 BURN STATUS REPORT
MNVR TO SIGHTING ATT
FLIGHT PLAN CMP
SM RCS CK
TRN BIAS
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
LMP
SPS MONITOR CK
INITIATE BAT CHARGE
MCC-14
09:30
MNVR TO PTC ATT
P 331 Y 331 P Y ROLL 0.1 ° /SEC
. STAR 16 ELDMK 10 LAT 28.876°N LONG/2 56.292 ° W ALT 000.01 STAR ELDMK LAT LONG/2 ALT
GROUND TRACK DET P21
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
12:00 CDR CMP
•
RECORD BLOCK DATA
LMP MCC-H
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
15:00 S F
SLEEP (7 HOURS
PERIOD
15:30 EAT PERIOD I EAT PERIOD
16:00
MISSION EDITION DATE TIME DAY" REV PAGE
AS503/103 FINAL November 22,1968 14:00 - 16:00 1 /TLC 2-13
MSC Form 1910 (Nov 69)
FLIGHT PLANNING BRANCH
0 0 ra •
• • • FLIGHT PLAN
16:00 CDR CMP
• LMP MCC—H
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
17:00 CDR
FLIGHT PLAN CMP LMP MCC—H
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 --
GROUND TRACK DET P21 17:45
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 • CDR
FLIGHT PLAN CMP MCC-I4
18:00
MNVR TO PTC ATT P 331 Y 331 P Y ROLL 0.1°/SEC
LiON CANISTER CHANGE (CARTRIDGE NO. 4 FROM A3 INTO CANISTER B)
18:30
19:00 5
N EAT PERIOD SLEEP PERIOD SLEEP PERIOD
(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
20:00 —
21:00 —
MSC Form 19I0 (Nov 98) FLIGHT PLANNING BRANCH
• S •
20:30 -
• •
21 30—
I 22: 0.0 -1
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 20:00 - 22 :00 1/TLC 2-17
FLIGHT PLAN CMP CDR LMP MCC -H
6
SLEEP PERIOD (7 HOURS)
SLEEP PERIOD (7 HOURS)
0 0 • • fi
CDR
FLIGHT PL AN CMP LMP MCC— H
22;00
22:30
23:00 F
SLEEP (7 HOURS)
PERIOD SLEEP (7 HOURS)
PERIOD
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
24:00 — CDR CMP IMP MCC-H
24:30 - SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)
25:00 - S 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
26:00— MNVR TO P52 ATT
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
26:00 CDR • CMP LMP
CMP/LMP CREW STATUS REPORT
MCC—H
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFT-- --
TORQUE ANGLES:
26:15 X
GDC ALIGN TO IMU TRN BIAS MNVR 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
0 •
MCC'S
BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC TRIM TO 0.2 fps
BURN STATUS REPORT
: I — ATIG
X X _ _ V g x
X X X
— 7 X X X. I ID
X X X y I V gx
j 9Y
; X X
X
X
X
. —r 1
X X
X
X
X
X 1
'REMARKS:
gz ;AV
C
FUEL
.0X
' UNBALANCE
CMP •
27:00 CDR
•
GROUND TRACK DET P21
27:15
V47 TRANS LM STATE VECTOR TO CSM SLOT EXT AV P30
SPS/RCS THRUST P40/41 MNVR TO BURN ATT
27:30
SXT STAR CK TRANS TO COUCH
27:45
TLI + 25 HRS
28:00
EMS AV TEST
GDC ALIGN MCC 2 AV=NOMINALLY ZER
SM RCS MON CK
MCC-H 6
P27 UPDATE: STATE VECTOR TGT LOAD
PIPA BIAS CK
IMP
•
0 0 is 0 O
S
FLIGHT PLAN
MISSION EDITION DATE TIME DAY/REV PAGE
1111/Miffill S503/103 FINAL ovember 22, 1968 __ ...„.... ...... ...• 27.:•00 — 2 • s1 •....... --.......... MSC Foim 1910 (Nov 68)
FLIGHT PLAN 28:00 --
CDR •
V66 TRANS CSM STATE VECTOR TO LM SLOT
CMP •
SM RCS MONITOR CK TRN BIAS
Liao •
SPS MONITOR CK INITIATE BAT CHARGE BIOMED Sw - RIGHT
MCC -H •
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
29:00 ]
P 331 Y 331
CDR CREW STATUS REPORT ROLL 0.1 °/SEC
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
CMP
LiOH CANISTER CHG (CARTRIDGE NO. 5 FROM A3 INTO CANISTER A)
LMP
EAT PERIOD I EAT PERIOD
UNSTOW TV CAMERA
T
MCC— H
COMM TEST MODE: 4
5 6 8 4,2 5.2 4,3 8.1 1.0 0.5 0,6 1.7 0.8 0,10
0 • 0 0 FLIGHT PL AN
29:00
29:30
30:00
31:00
30:30
S F N
CDR
SLEEP PERIOD (7 HOURS)
■.•
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
CDR 31:00
FLIGHT PL AN CMP LAW
BIOMED Sw - CENTER
MCC-H
TV
31:30
STOW TV CAMERA
32 :00 SLEEP PERIOD (7 HOURS)
32:30
33:001
•
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
CMP •
MCC-H CDR LMP
33:00
33:15
33:30 SLEEP PERIOD (7 HOURS)
33:45 MNVR TO P52 ATT
34:00
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF
— -- " —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
MCC—H
VOICE UPDATE: BLOCK DATA
•
FLIGHT PLAN CMP •
TORQUE ANGLES: X Y
LMP CDR 34:00 --
BIOMED Sw - RIGHT
SCT STAR VISIBILITY TRN BIAS MNVR TO SIGHTING ATT
34:15 -
ICISLUNAR NAVIGATION P23
. STAR 16 EFH STAR E H
1 SET
34:30 -" . STAR 22 EFH STAR E H
1 SET
SLEEP PERIOD (7 HOURS)
STAR 26 ENH STAR E H 1 SET 34:45 -
GROUND TRACK DET P21
RECORD BLOCK DATA (TLI + 35 HOURS, TLI + 44 HOURS, AND FLY BY)
MNVR TO PTC ATT P 331 Y 331 P Y ROLL 0.1°/SEC
1
-.135:00 •
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
SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)
REPORT T
35:00
35:30
36:00 F N
36:30
37:00
EAT PERIOD EAT PERIOD
CMP/LMP CREW STATUS
BIOMED Sw - LEFT
SLEEP PERIOD (7 HOURS)
EAT PERIOD
0 0 0 FLIGHT PLAN
CDR
CMP
LMP
MCC—H
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
CMP LMP MCC—H
SLEEP PERIOD (7 HOURS)
SLEEP PERIOD (7 HOURS)
FLIGHT PLAN 37:00
CDR
CDR CREW STATUS REPORT
37:30
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
CDR
FLIGHT PLAN CMP LMP MCC—H
39:00
39:3
40:00
40:30
SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)
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
41:00
FLIGHT PLAN CMP LMP MCC—H
I
41:30
42:00
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
•
CDR •
M S F N
SLEEP PERIOD (7 HOURS)
SLEEP PERIOD (7 HOURS)
MSC Form 7910 (Nov 08 ) FLIGHT PLANNING BRANCH
411 0 0
FLIGHT PLAN CMP CDR LMP MCC —H
43:00
S
N
43:30
44:00
MSC Form 1910 (Nov 613) ELI
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 43:00 - 44:00 2/TLC 2-31
EAT PERIOD I EAT PERIOD
BIOMED Sw - CENTER
EAT PERIOD
RECORD BLOCK DATA (TLI + 44 HOURS, FLY BY, PC 2 (QUICK RETURN), & PC + 2)
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DiFF --
TORQUE ANGLEST— -- X Y
44:00 —
•
44:30 —
.11
45:00 -1
CDR •
MNVR TO P52 ATT
GDC ALIGN TO IMU
CMP MCC-H 6
VOICE UPDATE: BLOCK DATA
S F N
LMP
CMP/LMP CREW STATUS REPORT
FLIGHT PLAN
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
CDR
MNVR TO SIGHTING ATT
FLIGHT PLAN CMP
•
TRN BIAS
CISLUNAR NAVIGATION P23
. STAR 33 LNH STAR L H
2 SETS
2. STAR 37 LNH STAR L H 1 SET
3. STAR 45 LFH STAR L H
1 SET
4. STAR 42 LFH STAR L H
1 SET
LMP
MCC—H • •
45:00 —
45:15 -
45:30 —
45:45
ti
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 - -
:X.X ! .ATIG — --
X X t BT 'V gx
X X X !
X XX'
_
I : ID
XXX ily V 9>c
V gY
V gz . A V
X X :X ;
)CX!Xi
X X !X
'REMARKS:
FUEL OX !UNBALANCE
C
MCC'S
BURN CHART
P or Y RATES
ATT. DEVIATION
SHUTDOWN TIME RESIDUALS .
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC TRIM TO 0.2 fps
• 0 0
• U
FLIGHT PLAN CMP
GROUND TRACK DET P21
SXT STAR CK
TRANS TO COUCH
LMP
BIOMED Sw - *RIGHT
RECORD MNVR PAD
MCC —H 6
P27 UPDATE: STATE VECTOR TGT LOAD VOICE UPDATE: MNVR PAD
PIPA BIAS CK
SM RCS MON CK
0 • 0
CDR
V47 TRANS LM STATE VECTOR TO CSM SLOT EXT AV P30
SPS/RCS THRUST P40/41
MNVR TO BURN ATT
EMS AV TEST
GDC ALIGN
1MCC 3 AV-NOMINALLY ZERO
46:00-•
46:15 -
,46:46-
LOI -22 FIRS 47:00--
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
47:00 imm
SPS MON CK INITIATE BAT CHARGE
CDR
MNVR TO SIGHTING ATT
V66 TRANS CSM STATE VECTOR TO LM SLOT
MCC i BURN STATUS REPORT
CMP
SM RCS MON CK
TRN BIAS
MCC—H
47:15
ICISLUNAR NAVIGATION P231
1. STAR 16 EFH STAR E H
1 SET
47:30
47:45 MNVR TO PTC ATT P 331 Y 331
ROLL 0.1°/SEC
2. STAR 22 EFH STAR E H
1 SET
3. STAR 26 ENH STAR E H
1 SET
GROUND TRACK DET P21
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
48:00 —
• 0 • 0 0
CDR •
LMP CMP •
MSC Form 1910 (Nov 613) FLIGHT PLANNING BRANCH
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
FLIGHT PLAN MCC—H
ti
FLIGHT PLAN CDR CMP
LMP
MCC—H 50:00
50:30
51:00 S 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
52:00 CDR CREW STATUS REPORT (cont'd) •
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
52:00 CDR CMP
TORQUE ANGLES: X
Z —
LMP
• 3IGMED Say - RIGHT
MCC-H
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
52:30 — S F N
SLEEP PERIOD (7 HOURS)
2 SETS
2. STAR 33 LNH
52:45 — STAR L H
3 SETS
••■
53:00 —
MISSION
AS503/103
EDITION
FINAL
DATE
November 22,1968
TIME
52:00 - 53:00
DAY/REV
3/TLC
PAGE
2-38 FLIGHT PLANNING BRANCH MSC Form 1910 (Nov 68)
FLIGHT PLAN 53:00
53:15
CDR CMP •
GROUND TRACK DET P21
LMP •
MCC-H
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
LMP
BIOMED Sw - CENTER UNSTOW TV CAMERA
MCC—H •
•
1'4 S F
0 0
CDR
FLIGHT PL AN CMP
54:00
54:15
SLEEP PERIOD (7 HOURS)
54:30
54:45
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
STOW TV CAMERA
•
FLIGHT PLAN
55:00 -- CMP LMP MCC—H
S
•
55:15-
, 1 T V
55 :30 —
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
CDR
1 S
SLEEP PERIOD F
(7 HOURS) N
56:00
56:30
57:00 5 F N
57:30
58:0
0 0 • CDR
SLEEP PERIOD (7 HO RS)
MCC—H • LMP
EAT PERIOD
•
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 56:00 - 58:00 3/TLC 2-42
FLIGHT PLAN CMP
EAT PERIOD
MSO Form 1910 (Nov 88) FLIGHT PLANNING BRANCH
FLIGHT PLANNING BRAN MSC Form 1810 (Nov 68)
CDR LMP MCC—H
FLIGHT PL AN CMP
58:00
58:30 SLEEP (7 HOURS)
PERIOD
59:00 SIOMED Sw - LEFT
59:30 EAT PERIOD P27 UPDATE: STATE VECTOR TGT LOAD REFSMMAT VOICE UPDATE
CDR CREW STATUS REPORT RECORD MNVR PAD MNVR PAD
60:00
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 58:00 - 60:00 3/TLC 2-43
X x X x
El TRIM_
X X X
IX X X
!XXX
BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC TRIM TO 0.2 fns
11 ATIG
BT V . gx
0 •
BURN STATUS REPORT MCC'S
V • gx
gY V
gZ 6V C
X X X FUEL X X X Ox X X X
. UNBALANCE
REMARKS:
60:00—
60:30—
60:45 , —
60:15-
61:00
FLIGHT PLAN CMP
IMU REALIGN P52 OPTION 1 - PREFERRED STAR ID STAR ANGLE DIFF
TORQUE ANGLES: X
Z
SXT STAR CK
TRANS TO COUCH
SM RCS MON CK
CDR
MNVR TO P52 ATT
EXT AV P30
SPS/RCS THRUST P40/41 MNVR TO BURN ATT
EMS AV TEST
GDC ALIGN TO IMU MCC 4 AV =. NOMINALLY ZER
LMP •
MCC —H 6
PIPA BIAS CK
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
• 61:00
CDR
V66 TRANS CSM STATE VECTOR TO LM SLOT
MNVR TO PTC ATT P 122 Y 315 P Y
61:15 ROLL 0.1 °/SEC
S 61:30 F
N
61:45
LMP MCC—H I
SPS MON CK INITIATE BAT CHARGE
ECS REDUNDANT COMP CK
CMP/LMP CREW STATUS REPORT
62:00
FLIGHT PLAN CMP
SM RCS MON CK
GROUND TRACK DET P21 (STATE VECTOR CK)
- • •
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
LMP CMP MCC—H
SLEEP PERIOD SLEEP PERIOD (6 HOURS) (6 HOURS)
62:00
62:30
63:00
63:30
64:00-1
CDR a
H
FLIGHT PL AN
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
SLEEP PERIOD (6 HOURS)
SLEEP PERIOD (6 HOURS)
0 • CDR
FLIGHT PL AN CMP LMP MCC—H
MNVR TO P52, ATT
MISSION EDITION DATE TIME DAY/REV PAGE
AS603/103 FINAL November 22,1968 64:00 - 66:00 3/TLC 2-47
64:00
64:30
S 65:00
F
65:30
66 : 00
MSC Form 19I0 (Nov Eli) FLIGHT PLANNING BRANCH
FLIGHT PLAN
66:00
CDR
CMP LMP MCC —H •
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF
TORQUE ANGLES: X Y
66:15
GDC ALIGN TO IMU
MNVR TO PTC ATT P 122 Y 315
ROLL O. 17YE0
66:30
SLEEP PERIOD (6 HOURS)
SLEEP PERIOD (6 HOURS)
66:45
RECORD MNVR PAD FOR LOI 1
VOICE UPDATE: MNVR PAD
67:00-1
MISSION' EDITION DATE TIME _ DAY/REV PAGE
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
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
67:00 --
67:15'
67:30 —
FLIGHT PLAN CMP
SLEEP PERIOD (6 HOURS)
LMP
SLEEP PERIOD (6 HOURS)
MCC—H
VOICE UPDATE: BLOCK DATA & MAP UPDATE 1/2
CDR •
MNVR TO LOI 1 ATT
SXT STAR CK
MNVR TO PTC ATT P 122 V 315 P ROLL 0.1c/SEC
RECORD BLOCK DATA (TEI 1' TEI 2' & PC+2)
& MAP UPDATE
MSC Form 1610 (Nov 68) FLIGHT PLANNING BRANCH
FLIGHT PL AN CMP
•
GROUND TRACK DET - P21 (LOI ALTITUDE DET)
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIF--
TORQUE ANGLES: X
SXT STAR CK
TRANSFER TO COUCH
68:00
68: 30 —
LMP •
CMP/LMP CREW STATUS REPORT
RECORD MANEUVER PAD
MCC-H 6
GO/NO GO
P27 UPDATE: STATE VECTOR TARGET LOAD
VOICE UPDATE: MNVR PAD
PRE LOI SYSTEMS CKS: C&W CK CM RCS CK SM RCS CK SPS PERIODIC MONITOR EPS PERIODIC MONITOR ECS PERIODIC MONITOR
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
CDR
GO/NO GO FOR LOI 1
MNVR TO P52 ATT
EXTERNAL AV P30 EMS CK SPS THRUST P40 MNVR TO BURN ATT
GDC ALIGN TO IMU
• 1111 •- di111
BURN STATUS REPORT
X X ATIG
X X BT
V gx TRIM
- X X X R
X X X P
X X X na
■_71 0
V
• vgx
gY
• V gz AV C
X X X FUEL
X X X ox
X X X UNBALANCE
0 •
LOI 1 BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME
RESIDUALS
LOI 1 10°/SEC TAKEOVER
10° TAKEOVER
B/T+6 SEC NO TRIM
LO1 1 ABORT MODES
LOI V90 BST TRAJECTORY ABORT MODE
3050-2100 0 -1:20 HYPERBOLIC COAST OUT OF SPHERE-P37 2100-1650 1:20-2:00 UNSTABLE 5 HR COAST. MODE I ABORT 1650-0 2:00-4:06 LUNAR ORBIT MODE III ABORT AFTER
1 REV
REMARKS:
FLIGHT PtANNI MSC Farm 1910 (Nov 08) • • • 0
FLIGHT PLAN CMP
• CDR
• • 69:00 --
SM RCS MONITOR CK
LOT1
GDC ALIGN TO IMU/ORB RATE (115 nm)
GO INERTIAL
ROLL RIGHT 180 0 AT 2°/SEC,_CONT INERTIAL ATT HOLD
LOI 1 BURN STATUS REPORT
GETI = 69:07:30 AV = 2991 fps BT = 4 MIN 5:8 SEC
V66 TRANS CSM STATE VECTOR TO LM SLOT
SM RCS MONITOR CK
2/80/83 4. 1/150/A8, R&B FILTER/U4, SPOT/ R13,INT/U4, 2 B&W FILM PACKS 1A8
UNSTOW ORBITAL CHARTS, 16/18/NEW C-EX/CABLE/ BRKT/U3
2/80/NEW B&W
EAT PERIOD
SPS MONITOR CK
INITIATE BAT CHARGE
CAMERA PREP
V64 ACQUIRE MSFN ON HGA
BEGIN REV 1 '
69:3
M S
N
LMP
BIOMED Sw - CENTER
MCC-H
ACQUIRE S/C
DUMP DSE
PIPA BIAS CK
• 70:00 --
16/18/NEW C EX, 1/250, SPOT, 1 FPS, (1 MAG)
EAT PERIOD
2/150/NEW B&W 1/250
1/80/B&W, 1/250
EAT PERIOD
MISSION EDITION DATE TIME DAY/REV PAGE
ASU3/103 FINAL November 221 196E, 69:00 - 70:00 3/LPO 2-51
• 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
EAT PERIOD STAR ID
-- 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
MAINTAIN ORB RATE AND BEGIN COAS GROUND TRACK DETERMINATION
YAW RT 45° FOR TV ORDEAL 180, 315, 45
TV
YAW LEFT 45° TO ORDEAL 180, 315, 0
CDR CMP
CONTROL PT (CP) SIGHTING (THRU HATCH WINDOW)
CP1 7 1 : 1 3: 4 6 TCA
CP1 NO. 504 LAT -05.250°S LONG -162.700°W ALT 000.00 nm
CP2 7 1: 2 7 : 4 0 TCA CP2 NO. 526 LAT -10.200°S LONG +155.100°E ALT 000.00 nm
CP3 7 1: 4 6: 3 TCA
CP3 NO. 334 LAT -09,100°S LONG +95.900°E ALT 000-.00 nm
PSEUDO LDG SITE LDMK SIGHTING (THRU HATCH WINDOW)
8
FLIGHT PLAN LMP
START 16 MM CAMERA AT TERMINATOR
SPOT METER READINGS
PHOTOGRAPH TARGETS OF OPPORTUNITY
CONFIGURE FOR TV
V64 ACQUIRE MSFN ON HGA
RECORD MAP UPDATE
MCC—H I
ACQUIRE S/C
P27 UPDATE: STATE VECTOR TARGET LOAD
VOICE UPDATE: MAP UPDATE 2/3
•
I 72:00
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 71:00 - 72:00 3/LPO 2-53
MSC Form 1810 (Nov 68) FLIGHT PLANNING BRANCH
•
0 • 0
72:00
72:10
FLIGHT PLAN CDR CMP
B-1 7 2: 0 9 : 1 0 AND COAS GROUND TRACK TCA1 MAINTAIN ORBITAL RATE
DETERMINATION LDMK NO. B1 LAT +02,675°N LONG +35.025°E ALT -000.99 nm
LMP MCC-H
GO/NO GO FOR L01 2
72:23
BIOMED Sw - LEFT STOP 16 MM CAMERA
RECORD MNVR PAD, BLOCK DATA (TEI 3 , TEI 3 NO LO1 2 )
GO/NO GO
VOICE UPDATE: MNVR PAD BLOCK DATA
LiOH CANISTER CHANGE (CARTRIDGE 9 FROM 85 INTO CANISTER A)
72:30 — IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , STAR ANGLE RIFF
1/80/HS, 1/4, F 2.8 DUMP DSE
•
EXTERNAL AV P30
EMS CK
SPS THRUST - P40
73:00 --
TORQUE ANGLES: — PRE LOI SYSTEMS CKS: X z _ C&W CK
CM RCS CK SPS PERIODIC MONITOR EPS PERIODIC MONITOR ECS PERIODIC MONITOR
PIPA BIAS CK
•
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
BURN STATUS REPORT ---; - 1-- - I
!X X. " 1ATIG 1- BT )<!)‹ *.._, i V gx
n 1 F_J
R
V • , gx
1V gY
V gz AV C
FUEL j)); :UNBALANCE
REMARKS:
0
LOI 2 BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
LOI 2 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC NO TRIM
3
0 0
73:00--
73:03 •
CDR
MNVR TO BURN ATT GO INERTIAL
73:09
73:17
GOC ALIGN TO IMU
GDC ALIGN TO IMU/ORB RATE (60 nm)
ROLL RIGHT 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC (HEADS OWN TRACKING ATT) ORDEAL 180, 308, 0 BEGIN ORB RATE
73:48 LOI 2 BURN STATUS REPORT
74:00
CMP •
SXT STAR CK
TRANSFER TO COUCH
BEGIN REV 3
SM RCS MONITOR CK
GETI = 73:30:54 AV = 138.5 fps BT = 9.7 SEC
V66 TRANS CSM STATE VECTOR TO LM SLOT
SM RCS MONITOR CK
REST PERIOD (2 HOURS)
0 • 0 • FLIGHT PLAN
LIMP
2/80/B&W, 1/250
16/18/C EX, 1/250 F CHART, 6 fps, BRACK
1/150/B&W, 1/60, CHART, BRKT
PRE LOI SYSTEMS CKS
SPS MONITOR CK
INITIATE BAT CHARGE
V64 ACQUIRE MSFN ON HGA
BIOMED Sw - RIGHT
MCC—H b
ACQUIRE S/C
PIPA BIAS CK
MISSION
AS503/103
EDITION
FINAL
DATE
November 22, 1962
TIME
73:00 - 74:00
DAY/REV
1 4/LPO
PAGE
2-55
MSC Fun 1910 (Nov 69) FLIGHT PLANNING BRANCH
CDR •
TRAINING PHOTOGRAPHY
PITCH UP TO TRACK LDMK
7 4 : 1 5 :
FLIGHT PLAN
74:17
LMP MCC—H •
'TRAINING PHOTOGRAPHY ,70mm & 16mm
START CAMERAS 7 MIN PRIO LDMK 70mm - 20 SEC INT UNTIL TRACKING - THEN 5 SEC F STOP FROM CHART
STOP CAMERA STOP CAMERAS
I 75:00 =I
PITCH DWN TO HEADS DWN TO REACQUIRE MSFN ORDEAL 180, 0, 0 GO INERTIAL
INSTALL 16 MM CAMERA
GDC ALIGN TO IMU
•
1/80/HS, 1/4, F 2.8
VERIFY SYSTEMS STATUS
RECORD MAP UPDATE
IMU REALIGN P52 OPTION 3 REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF
TORQUE ANGLES: X Y
RECORD BLOCK DATA (TEI 3 & TEI 4 )
a
VOICE UPDATE: MAP UPDATE 3/4
DUMP DSE
VOICE UPDATE: BLOCK DATA •
CMP
REST PERIOD (2 HOURS)
r"-̂ ",„,,o
MISSION EDITION DATE TIME DAY/REV PAGE
AS5L3/103 LINAI November 22, 1968 74:00 - 75:00 4/LPO 2-56
MSC Form 1810 (Nov 88) FLIGHT PLANNI
CDR CMP LMP
1/80/NEW B&W, 1/250, F 2.8 BRKT/INT
2/150/B&W
START CAMERA 1 S/C SR 6 MIN
PITCH UP TO VERTICAL AT 0.2°/SEC (+Z FWD) ORDEAL 180, 270, O. BEGIN ORB RATE
16/18/NEW C EX/1 fps 1/250, F 2, 1 fps START CAMERA S/S SR 4- 6 MIN
SUBSOLAR POINT
75:46
ROLL RIGHT 180° AT 2°/SEC (-Z. FWD) MAINTAIN ORB RATE
REST PERIOD (2 HOURS)
INSTALL SXT BRKT & 16mm CAMERA. TAKE PHOTOS AS TIME PERMITS,
75:30
BEGIN REV 4
75:46
SA 0° TA 0 °
76:00
MCC—H U
ACQUIRE S/C
• 75:00
75:15
75:09
VERTICAL STEREO PHOTOGRAPHY
EXTRA EXP EACH 5 MIN - NOTE TIME
ACQUIRE MSFN ON QMNI ANT
FLIGHT PL AN
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
76:21
FLIGHT PLANNING BRANCH MSC Form 1910 (Nov 68)
• 0
CDR 76:0
PITCH UP AT 0.2°/SEC TO 0, 35, 5, 0
BEGIN ORB RATE
STOP CAMERAS AT TERMINATOR 76:15
76:30 —1
S F
ROLL RIGHT 180° AT 2°/SEC (HEADS DWN) GO INERTIAL
EAT PERIOD
GDC ALIGN TO IMU
76:58 77:00
FLIGHT PLAN CALF
T
IPI .
• ACQ . .
. IPII . . •
ACQ . .
{LDMK LIGHTING EVALUATION (THRU OPTICS) OF LDMK 81
IMU REALIGN OPTION 3 - REFSMMAT AND GYRO DRIFT STAR ID STAR ANGLE DIFF
TORQUE ANGLE S : X Y
P52
TEST
, — --
Z .
1
V64 ACQUIRE MSFN ON HGA
1/80/HS, 1/4, F 2.8 '(20 SEC STRIP - 20 EXP)
VERIFY SYSTEMS STATUS
RECORD BLOCK DATA: (TEI 4 & TEI 5 )
TRANS TO LEFT COUCH
1/80/B&W, 1/250, F 2.8 INT (CDR).
BIOMED Sw - CENTER
MISSION EDITION DATE TIME DAY/ REV PAGE
AS503/103 FINAL November 22, 1968 76:00 - 77:00 4/LPO 2-58
LMP
AT PITCH UP 1/80/B&W, 1/250, F 11
STOP CAMERA 1 AT TERM
RECORD MAP UPDATE
MCC-H
VOICE UPDATE: MAP UPDATE 4/5 P27 UPDATE: STATE VECTOR
ACQUIRE S/C
DUMP DSE
VOICE UPDATE: BLOCK DATA
MSC Form 1910 (Nov 88) FLIGHT PLANNING BRANCH
0 FLIGHT PLAN
CMP LMP
ROLL LEFT 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE.
2/150/B&W, 1/250 F 2.8
2/150/B&W, 1/250 (CDR)
PITCH DWN AT 0.3°/SEC AT ACQ
ACQUIRE MSFN ON OMNIS AT LOSS PITCH UP AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE.
REPORT NEW CP COORDINATES
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 77:00 - 78:00 4/LPO 2-59
CDR
77:08
77:14
77:00 •
EAT PERIOD
BEGIN REV 5
77:30
77:44
REST PERIOD (3 HOURS)
78:00
MCC -H ti
ACQUIRE S/C
MAP REVIEW
P22 MANUAL ACQ SA 0°, TA 10°
I CNTL POINT SIGHTING
IP I ACQ
CP2 NO. 526 LAT -10.200°S LONG/2 +77.550 °
ALT +000.00 nm
NEW COORDINATES LAT LONG/2 ALT nm
REVIEW LDMK MAP
FLIGHT PLAN CMP
•
PSEUDO LDG SITE SIGHTINGS P22 - AUTO OPTICS IPI TCA LDMK NO, 81 LAT +02.675°N LONG/2 +17.512° ALT -000.99 nm NEW COORDINATES LAT + LONG/2 + ALT
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF--
TORQUE ANGLES: X Y z .
LMP
PITCH DWN 0.3°/SEC AT ACQ
AT LOSS ROLL RIGHT 180° AT 2°/SEC TO HEADS DWN GO INERTIAL
V64 ACQUIRE MSFN ON HGA 1/80/HS, 1/4, F 2.8
REPORT NEW COORDINATES
RECORD BLOCK DATA (TEI 6 ), & MAP UPDATE
VERIFY SYSTEMS STATUS
GDC ALIGN TO IMU 16/18/ C EX, 1/250, 1 fps
MAGS)
2/150/C121/1/250 SPOT GENERAL OBSERVATIONS
a
CDR
REST PERIOD (3 HOURS)
0
n
MCC—H 6
ACQUIRE S/C
P27 UPDATE: STATE VECTOR VOICE UPDATE: BLOCK DATA
MAP_ UPDATE 5/6
DUMP DSE
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL Novemb e r 22, 1968 78:00 - 79:00 4/LPO 2-60
MSC Form 1910 (Nov 68) FLIGHT PLAN
• 0 ti •
0 0 • 1 0 FLIGHT PLAN
CMP LMP
REVIEW CONTROL POINT MAP ROLL 180° AT 2°/SEC PITCH DWN AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE
PITCH DWN 0.3°/SEC AT AC
T LOSS PITCH UP 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° ALT +000.00 nm
NEW COORDINATES LAT 0 LONG/2 ALT nm
REVIEW LDMK MAP CQUIRE MSFN ON OMNIS
REPORT NEW COORDINATES
'PSEUDO LDG SITE SIGHTING!
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 79:.00 - 80:00 4/LPO 2-61
CDR
REST PERIOD (3 HOURS)
•
ACQUIRE S/C
MCC—H S
MSC Form 1910 (Nov Ea) FLIGHT PLANNING BRANCH
CDR 80:00
80:13
REST PERIOD (3 HOURS)
ROLL LEFT 180° AT 2°/SEC PITCH UP AT 0.2°/SEC TO ORDEAL 0, 5, O. BEGIN ORB RATE
0:19
FLIGHT PLAN LPAP
MCC—H CMP
P22 AUTO OPTICS IPII TCAI LDMK NO. B1 LAT +02.675°N LONG/2 +17.512° ALT -000.99 nm NEW COORDINATES LAT LONG/2 0
ALT
nm
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , STAR ANGLE DIFF
TORQUE ANGLET— -- X y
16/SXT/NEW C XT, 6 fps
•
PITCH DWN 0.3°/SEC AT ACQ
AT LOSS ROLL RIGHT 180° AT 2°/SEC. GO INERTIAL
V64 ACQUIRE MSFN ON HGA ACQUIRE S/C P27 UPDATE: STATE VECTOR VOICE UPDATE: BLOCK DATA & MAP
VERIFY SYSTEMS STATUS DUMP DSE UPDATE 6/7
1/80/B&W, 1/250 F 2.8 IN
2/150/B&W, 1/250 (R&B)
TRANS TO RIGHT COUCH
EAT PERIOD
REPORT NEW COORDINATES
RECORD BLOCK DATA (TEI 7 )& MAP UPDATE
MISSION EDITION DATE TIME DAY/REV f PAGE
AS503/103 FINAL November 22, 1968 80:00 - 81:00 4/LPO 2-62
MSC Form 1910 (Nov 88)
FLIGHT PLANNING H
• 0 14 ,
0 • 0 •
EAT PERIOD
NEW COORDINATES LAT LONG/2 ALT
0
nm
FUG MSC Form 1910 (Nov 68)
CDR
PITCH DWN AT 0.3°/SEC AT ACQ
AT LOSS PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0
PITCH DWN AT 0.3°/SEC AT ACQ
T LOSS PITCH UP AT 0.5°/SEC TO RDEAL 0, 5, 0
PITCH OWN AT 0.3°/SEC AT CQ
AT LOSS PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0
81:00--
81:05 -
81:11 -
FLIGHT PLAN CMP
ICNTL PT SIGHTINGS (3)1
P22 MAN ACQ SA 0° TA IPI ACQ
-- CP1 NO. 504-- LAT -05.250°S LONG/2 -81.350° ALT +000.00 nm
10°
P22 AUTO OPTICS IPI I TCA 1 ' --
CP2 NO. 526 LAT -10.200°S LONG/2 +77.550 ° ALT +000.00 nm
P22 MAN ACQ SA 0° TA 10° IPI I ACQ
• I . CP3 NO. 334 - LAT -09.100°S LONG/2 +47.950° ALT +000.00 nm
'PSEUDO LOG SITE SIGHTING'
P22 AUTO OPTICS
LMP
BIOMED Sw - LEFT
T EAT PERIOD
NEW COORDINATES LAT LONG/2 ALT nm
NEW COORDINATES LAT LONG/2 . ° ALT nm
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 81:00 - 82:00 4/LPO 2-63
MCC—H
ACQUIRE 5/C
REST PERIOD (2 HOURS)
ACQUIRE S/C P27 UPDATE: STATE VECTOR VOICE UPDATE: MAP
8 UPDATE
BLOCK DATA DUMP DSE
FLIGHT PLAN CMP
• MCC—H LMP
82:53 — I
83:00 • I
PITCH DWN AT 0.3°/SEC AT ACQ
AT LOSS ROLL RIGHT 180° AT 2°/SEC GO INERTIAL
ACQUIRE MSFN ON HGA
REPORT NEW COORDINATES
RECORD MAP UPDATE & BLOCK DATA (TEI 8 )
GDC ALIGN TO IMU
ROLL LEFT 180° AT 2°/SEC TO HEADS UP
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
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE IF !J F--
TORQUE ANGLES: X Y Z
16/SXT/CXT„6 fps
82:00 —
82:11
82:17
82:30 —
0
nm
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103, FINAL November 22, 1968 82:00 - 83:00 4/LPO 2-64
MSC Form 1910 (Nov 08) FLIGHT PLANNI
0 0 0 0
0 • • 0
FLIGHT PLANNING BRANCH
CDR
PITCH DWN AT. 0.2°/SEC TO ORDEAL 0, 5, 0
3:00
83:03
83:10
PITCH DWN AT 0.3°/SEC AT ACQ
EGIN REV 8
AT LOSS PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0
PITCH OWN AT 0.3°/SEC AT ACQ
PITCH UP AT 0.5 ° /SEC TO ORDEAL 0, 5, 0
ACQUIRE MSFN ON OMNIS .
83:30
83:39
PITCH OWN AT 0.3°/SEC AT ACQ
PITCH UP AT 0.5°/SEC TO ORDEAL 0, 5, 0
84:00
FLIGHT PLAN CMP
ICNTL PT SIG}-TINGS (3)
P22 11)1 TCA CP1 LAT LONG/2 ALT
AUTO OPTICS __. .._, __ __
NO. 504 -05.250°S -81.350° +000.00 nm
P22 AUTO OPTICS IPI . TCA .• CP2 NO. 526 LAT -10.200 ° S LONG/2 +77.550° ALT +000.00 nm
P22
TCA CP3 LAT LONG/2 ALT
IPII AUTO OPTICS
• NO. 334 • -09.100°S +47.950 ° +000.00 nm
PSEUDO LOG SITE SIGHTINGI
P22 AUTO OPTICS
LMP
REST PERIOD (2 HOURS)
NEW COORDINATES LAT LONG/2 ALT nm
NEW COORDINATES LAT LONG/2 0
ALT nm
0
nm
MISSION EDITION DATE TIME DAY, REV PAGE
AS503/103 FINAL November 22, 1968 83:00 - 84:00 4/LPO 2-65
NEW COORDINATES LAT LONG/2 ALT
MCC-H ti
ACQUIRE S/C
•
MSC Form 1910 (Nov 68)
nm
NEW COORDINATES LAT LONG/2 ALT
FLIGHT PLANNING BRANCH MSC Form 1910 (Nov 58)
0 • 0
84:0
PITCH DWN AT 0.3°/SEC AT ACQ
AT LOSS ROLL RIGHT 180° AT 2°/SEC (HEADS DWN) GO INERTIAL
ACQUIRE MSFN ON HGA
DC ALIGN
PITCH UP AT 0.2°/SEC TO ORDEAL 180, 0, 0 (HEADS DWN) BEGIN ORB RATE
16/18/NEW CEX, 1/250, f2.8, 1 fps
•
84:10
84:16
84:30 —
84:51
85: 00 -I
FLIGHT PLAN CMP
• IPI TCA
I
LDMK NO. 81 LAT +02.512°N LONG/2 +17.512° ALT +000.99 nm
LION CANISTER CHANGE (CARTRIDGE 10 FROM B5 INTO CANISTER B)
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , _ STAR ANGLE DIFF
TORQUE ANGLES: X
z
REST PERIOD (2 HOURS)
LMP
REST PERIOD (2 HOURS)
1 2/150/NEW B&W, 1/250 (R&B)
BIOMED Sw - RIGHT
VERIFY SYSTEMS STATUS
RECORD MAP UPDATE & BLOCK DATA (TEI 9 )
1/80/H.S. B, f2.8, POL
SR -12 MIN START DARK
1/80 B&W, 1/4, f4,POL
SR -4 MIN START CORONA •
MISSION I DITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 84:00 - 85:00 4/LPO 2-66
VOICE UPDATE: MAP UPDATE 8/9 BLOCK DATA
ACQUIRE S/C
P27 UPDATE: STATE VECTOR
DUMP DSE
MCC—H I
LMP •
1/80/NEW C BRKT INT
START CAMERA I AT SR +12 MIN
ACQUIRE MSFN ON HGA
RECORD MAP UPDATE
2/80 B&W/R&B 4 STOPS WIDER
MCC—H • CDR
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
85:00 85:0
85:08
BEGIN REV 9
ZERO PHASE TARGETS OF OPPORTUNITY
REST PERIOD (2 HOURS)
85:30
86: 00
85:3 ACQUIRE S/C
VOICE UPDATE: MAP UPDATE 9/10
CMP •
PITCH UP 40° AT 0.2°/SEC TO ORDEAL 180, 260, 0
] ROLL RT AS REQD TO SHADE WINDOWS-KEEP X-AXIS +10° ON TRACK
TV
CONVERGENT STEREO PHOTOGRAPHY-EXTRA EXP EACH 5 MIN - NITE TIME
• ,4r
FLIGHT PL AN
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 85:00 - 86:00 4/LF0 2-67
MSC Farm 1910 No 6 8) FLIGHT PL N I
ri
CDR •
STOP CAMERA AT TERM
ROLL RIGHT 180° IF REQD PITCH DWN 60° AT 0.2°/SEC TO ORDEAL 180, 310, 0 (HEADS DWN) GO INERTIAL
PITCH DWN AT 0.2°/SEC TO ORDEAL 180, 180, 0 BEGIN ORB RATE (HEADS DWN +Z FWD)
•
REST PERIOD (2 HOURS)
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , STAR ANGLE DIFF
TORQUE ANGLEST----- x
Y
STOP CAMERA AT TERM 2/80/HS, 1/4 f2.8
RECORD BLOCK DATA (TEI 10 ) & MNVR PAD
VERIFY SYSTEMS STATUS
1/80/NEW B&W 1/250, f2.8 INT (CDR) 2/150/C, 1/250
P27 UPDATE: STATE VECTOR
VOICE UPDATE: BLOCK DATA MNVR PAD
DUMP DSE I
FLIGHT PLAN CMP MCC—H
I LMP
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL iNovember 22, 1968 86:00 - 87:00 4/LPO 2-58
MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH
0 0
CDR CMP LMP •
MNVR TO TEI ATT
PITCH UP AT 0.2°/SEC TO ORDEAL 180, 180, 0 BEGIN ORB RATE
EAT PERIOD
BEGIN REV 10
SXT STAR CK
EAT PERIOD EAT PERIOD
2/150/B&W OR 0,1/250
ACQUIRE MSFN ON HGA
RECORD MNVR PAD, BLOCK DATA (TEI 11 ), MAP UPDATE
-1'
• FLIGHT PLAN
MCC—H •
ACQUIRE S/C
DUMP DSE PIPA BIAS CK P27 UPDATE: STATE VECTOR TARGET LOAD
VOICE UPDATE: MNVR PAD BLOCK DATA 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 PLANNING BRANCH MSC Form 1910 (Nov 68)
(4 • •
FLIGHT PLAN CDR
GO/NO GO FOR TEI
88:07
88:13
88:30 —
EXTERNAL AV P30 EMS TEST SPS THRUST P40
MNVR TO BURN ATT
PUGS MODE Sw - AUX
88:00 — CMP
•
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID STAR ANGLE DIFF
TORQUE AGES
Y
SXT STAR CK
TRANSFER TO COUCH
LMP
2/150/C SPOT 16/75/CEX/1 fps/SPOT
PRE TEI SYSTEMS CKS
C&W CK CM RCS CK SM RCS CK SPS PERIODIC MONITOR EPS PERIODIC MONITOR ECS PERIODIC MONITOR
MCC—H
GO/NO GO BIOMED Sw -LEFT
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 88:00 - 89:00 _ 4/LPO 2-70
BURN STATUS REPORT
X I X ATIG X X BT
•t V gx
T RIM
>XXi 1
XI X X
)()<>0 ! IY V gx V
gY t T-Vgz
C
FUEL
. !Ox - 'UNBALANCE
X XIX
X X A Xt i 'X X:Xi
REMARKS:
0 0
TEI BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
TEl 10 ° /SEC TAKEOVER
10° TAKEOVER
B/T+2 SEC & AV
c-40 fps
TRIM TO 2,0 fps
TEI ABORT MODES-SYSTEMS PROBLEMS:15-MIN ABORT CHART OTHERWISE
TEI V qo B/T TRAJECTORY ABORT MODE
2850-950 0 -2:00 LUNAR ORBIT MODE III AFTER 1 REV 950-600 2:00-2:20 UNSTABLE 5-HR COAST, MODE I 600-0 2:20-2:54 HYPERBOLIC COAST OUT OF SPHERE - P37
89 : 0 0
89:76 -
89:30 —
ml
89:45 -
I 90:00 :I
FLIGHT PLAN CMP
• LMP MCC—H
• CDR
•
GDC ALIGN TO IMU
iTEII
PITCH UP TO VERTICAL +Z FWD) TO ACQ MOON
IN WIND W CDR CREW STATUS REPORT
SLEEP PERIOD (5 HOURS)
SM RCS MON CK
GETI = 89:15:07 AV = 3532 fps BT = 3, MIN 26 SEC
SM RCS MON CK
TRANS CSM STATE VECTOR TO LM SLOT
REINITIALIZE W MATRIX R
1 +00094
R 2 +00571
R 3 +00003
SPS MON CK
ACQUIRE MSFN WITH HGA
TEI BURN STATUS REPORT INITIATE BAT CHARGE
BIOMED Sw - CENTER
•
ACQUIRE S/C
DUMP DSE UPDATE ENTRY REFSMMAT
•
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
MCC— H
•
0 • 90:00 --
FLIGHT PLAN LMP
•
0 LMP
•
MNVR TO P52 ATT
90:15-
90:30
IMU REALIGN P52 OPTION 1 - PREFERRED STAR ID STAR ANGLE DIF —
TORQUE ANGLET- -- X
TRN BIAS
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
•
CDR
SLEEP PERIOD (5 HOURS)
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
CDR LMP MCC—H
FLIGHT PLAN .
CMP
MSC Form 1910 (Nov 08) FLIGHT PLANNING BRANCH
0
91:00
91:15 TRN
3.
BIAS
STAR 10 STAR
LFH L H
MNVR TO SIGHTING ATT
2 SETS
91:30 F SLEEP PERIOD (5 HOURS)
4. STAR 11 LFH STAR L H
91:45 2 SETS
92:00
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 91:00 - 92:00 4/TEC 2-73
0 • 0 FLIGHT PL AN
LMP •
MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0,1°/SEC
MCC—H I 92:00
92:15
92:30
92:45
i93:0
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
CDR
OAP e•-11L—i •
S F
SLEEP PERIOD (5 HOURS)
CDR CMP CMP MCC—H
MSC Farm 1910 (Nov BB)
• 0 0 0
FLIGHT PLANNING BRANCH
•
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
AS503/103 FINAL November 22, 1968 93:00 - 95:00 4/TEC 2-75
FLIGHT PLAN
0 • 0 '0 FLIGHT PLAN
95:00_ • CDR
• CMP thiP MCC—H
I
CDR CREW STATUS REPORT
95:15 -
95:30 —
S F
SLEEP (5 HOURS)
PERIOD SLEEP (5
PERIOD 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
96: 00 —
96:75
CDR CMP LMP MCC-H I
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DI FF---
TORQUE ANGLES:
X
Y
MNVR TO PTC ATT P 029 Y 315
ROLL 0.17TEC SLEEP PERIOD SLEEP PERIOD 96:30 — (5 HOURS) (5 HOURS)
96:45 —
:1 I
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22, 1968 96:00 - 97:00 5/TEC 2-77
MSC Form 1910 (Nov E8)
FLIGHT PLANNING BRANCH
97:00
0
0 0 • • • CDR
FLIGHT PLAN 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
AS503/103 FINAL November 22, 1968 97:00 - 99:00 5/TEC 2-78
MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH
FLIGHT PL AN CDR CMP
99:30 —
99:15 -
99:00 —
EAT PERIOD I EAT PERIOD
LMP MCC—H
BIOMED Sw - , CENTER ENTER
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
100:00 CDR
MNVR TO P52 ATT
CMP LMP
CMP/LMP CREW STATUS REPORT
MCC—H
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 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
S503 103 FINAL November 22, 1968 100:00 - 101:00 5/TEC 2-80
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
102:00 CDR CMP LMP MCC—H
I
3 . STAR 31 ENH STARE H 2 SETS --
102:15
P27 UPDATE STATE
102:30 VECTOR 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 ' S
BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC TRIM TO 0.2 fos
BURN STATUS REPORT
X
X
X tTIG
,BT V gx
X
----7TRIM _ X X X R X X X P
'XXX V gx V
;\) 1 coI.)
....+ _. 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 ,
103:00 CDR CMP
• LMP
• MCC —H
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 -- • V66 TRANS CSM STATE MCC 5 BURN STATUS REPORT
I
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 —
105:00 —1 CDR CREW STf TUS REPORT
MISSION EDITION DATE TIME DAY/REV PAGE
1111/111111111/111111 AS503/103 FINAL November 22 1968 104:00 - 105:11 MSC Form 1910 (Nov 68)
FLIGHT PLANNING BRANCH
• 0 0
M S F N
CDR
SLEEP PERIOD (7 HOURS)
0 0 0 FLIGHT PLAN
crow •
LiOH CANISTER CHANGE (CARTRIDGE NO. 12 FROM B6 INTO CANISTER 13)
LMP •
BIOMED Sw - CENTER TRANS TO LH COUCH MNVR TO SIGHTING ATT
MCC—H 6
TRN BIAS
CISLUNAR NAVIGATION P23
1. STAR 22 EFH STAR E H
2 SETS
2. STAR 26 ENH STAR E H
1 SET
105:00--
105:15 -
105:30 —
105:45 -
3 . STAR 31 ENH STAR E H
2 SETS •
106:00--
MISSION EDITION DATE TIME DAY/REV PAGE
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
106:30 S SLEEP PERIOD STAR L H
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
CDR
107:00
107:15
S 107:30
F N
1 07:45
108:00
SLEEP PERIOD (7 HOURS)
LIMP
MNVR TO P52 ATTITUDE
MNVR TO SIGHTING ATT
MCC—H •
•
• 41 • 0 I .
FLIGHT PLAN
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DEFT
TORQUE ANGLES:
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
108:00 -- CMP LMP
• •
CISLUNAR NAVIGATION P231 BIOMED Sw - RIGHT
1. STAR 22 EFH STAR E H 1 SET
MCC—H •
108:15 -
2. STAR 26 ENH STAR E 2 SETS --
1 108: 30—
-I
108:45
109:00 :1
3. STAR 31 ENH STAR E H 2 SETS
RETURN TO EARTH P37
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
CDR
SLEEP PERIOD (7 HOURS)
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
MCC—H •
•
0 • CDR
SLEEP PERIOD (7 HOURS)
LMP •
•
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 109:00 - 111:00 5/TEC 2-89
FLIGHT PLAN CMP
109:00
109:30
H S
1 10:0 0
F N
110: 3 0
111:00
MSC FLIrm 1910 (Nov 6$) FLIGHT PLANNING BRANCH
SLEEP PERIOD (7 HOURS)
FLIGHT PLAN CDR
CMP LMP
MCC— H
EAT PERIOD I EAT PERIOD
CMP/LMP CREW STATUS REPORT
BIOMED Sw - LEFT
SLEEP PERIOD (7 HOURS)
111:00
111:30
112:00
112:30
113:00 -I MISSION EDITION DATE TIME DAY/ Inv PAGE
AS503/103 FINAL November 22, 196e 111:00 - 113:00 5/TEC L 2-90
MSC Form 1910 (Nov 58) FLIGHT PLANNING BRANCH
SLEEP PERIOD (7 HOURS)
EAT PERIOD
0 0
0 • • 4• FLIGHT PLAN
CDR CMP LMP MCC-H
113:00 f
CDR CREW STATUS REPORT
113:30 -
.M1
114:00 — S F N
SLEEP (7 HOURS)
PERIOD SLEEP (7 HOURS)
PERIOD
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
115:00
115:15
115:30
115:45
i116:00
CMP
SLEEP PERIOD (7 HOURS)
L PAP
SLEEP PERIOD (7 HOURS)
MCC—H 4
CDR
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE DIFF
TORQUE ANGLES: X Y
MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1 °/SEC
FLIGHT PLAN
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
• • FLIGHT PL AN
CDR
CMP
LMP
MCC-H
0 0 116:00
116:30
117:00
117:30
118:00
SLEEP PERIOD (7 HOURS)
SLEEP PERIOD (7 HOURS)
•
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
•
M S F N
118:00 —
118:30 -
CDR
EAT PERIOD
FLIGHT PLAN CMP L MP MCC ..-14
S
LiOH CANISTER CHANGE (CARTRIDGE NO. 13 FROM B6 INTO CANISTER A)
MNVR TO SIGHTING ATT
119:00 —
119:30 —
1
120:00 •
SLEEP PERIOD SLEEP PERIOD (7 HOURS) (7 HOURS)
EAT PERIOD
TRN BIAS
BIOMED S - CENTER
EAT PERIOD
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
120:00 - CDR CMP
• LMP
• MCC—H
•
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 SE -7- —
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 CHART
P or V RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
B/T +1 SEC TRIM TO 0.2 fns
BURN STATUS REPORT
X X •
_ATIG
X X • BT
V gx
TRIM. X X X
R
X X X
P
X X X
Y V
gx V
V gY
c)
9.2 AV c
X X X FUEL
X X X Ox
X X X UNBALANCE
REMARKS:
• 0
0 • ' FLIGHT PL AN
121:00 CDR
• CMP
• LMF MCC—H
•
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 122:00
CDR
V66 TRANS CSM STATE VECTOR TO LM SLOT
CMP
SM RCS MON CK
LMP
MCC 6 BURN STATUS REPORT
INITIATE BAT CHARGE
MCC—H I
STONED Sw - RIGHT
MNVR TO SIGHTING ATT
122:15
122:30
122:45
I
123:00
TRN BIAS
1CISLUNAR NAVIGATION P231
1. STAR 02 LNH STAR L H 2 SETS
2. STAR 01 LNH STAR L H 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
CDR
FLIGHT PLAN CMP OAP MCC—H
123:00 • •
RETURN TO EARTH P37
MNVR TO SIGHTING ATT
123:30
123:30 F N
TRN BIAS
[CISLUNAR NAVIGATION P231
1. STAR 22 EFH STAR E H
123:45 2 SETS —
2. STAR 26 ENH STAR E H
124:00 1 SET •
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
124:00 —, CDR CMP 1MP MCC—H
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
• 0 • 0 0
MSC Form 1910 (Nov 68)
FLIGHT PLANNING BRANCH
• 0 • • FLIGHT PLAN
125:00 -- • CDR •
CMP LMP
BIOMED Sw - CENTER
MCC—H •
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
CDR CMP
SLEEP PERIOD (7 HOURS)
FLIGHT PLAN
127:00 — LMP
LiOH CANISTER CHANGE (CARTRIDGE NO. 14 FROM B6 INTO CANISTER B)
MCC—H
127:30
11.
BIOMED Sw - RIGHT
UNSTOW TV CAMERA
128:00 —
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
• 129:00 —
129:15 -
M S F N
129:30 —
129:45 -
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22,1968 129:00 - 130:00 6/TEC 2-102
FLIGHT PLANNING BRANCH
130:00-- •
MSC Form 1910 (Nov 68)
FLIGHT PLAN CMP
• LMP
• MCC —H
I
SLEEP PERIOD (7 HOURS)
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID , STAR ANGLE 15-I-FF --
TORQUE ANGLE S :
Y X
TRN BIAS
MNVR TO P52 ATT
MNVR TO SIGHTING ATT •
CDR
FLIGHT PLAN
130:00 — CDR CMP
• LMP MCC—H
CISLUNAR NAVIGATION P23 '
STAR 02 LNH STAR_
— H
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
CDR
SLEEP PERIOD (7 HOURS)
S F N
0 0 FLIGHT PLAN
CMP LMP
BIOMES Sw - CENTER
MCC-H 6
131 :00
131 :15
131 :30
2. STAR 26 ENH STAR E H 2 SETS
3. STAR 31 ENH STARE H 2 SETS --
131:45
132:00 RETURN TO EARTH P37
MNVR TO PTC ATT P 029 Y 315 P Y ROLL 0.1°/SEC
•
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
STATE VECTOR GO/NO GO RECORD BLOCK DATA FOR EI -2 HOURS
1 3 4:00 -1
11SC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH
• 0 0 e0
CMP LMP MCC—H
EAT PERIOD I EAT PERIOD
132:00
13230
EI -15 HRS .
P27 UPDATE: STATE VECTOR GO/NO GO VOICE UPDATE: BLOCK DATA FOR EI -2 HOURS MCC
CDR
SLEEP PERIOD (7 HOURS)
133:00
133:30
CMP/LMP CREW STATUS REPORT
BIOMED Sw - _LEFT
MISSION PAGE EDITION DATE TIME DAY/REV
AS503/103 FINAL November 22,1968 132:00 - 134:00 6/TEC 2-10 5
• • • 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 136:00 — s.
136:30 -
SLEEP PERIOD M (7 HOURS)
137:00 — S F
137:30 -
•
138:00 —
LMP MCC—H
SLEEP PERIOD (7 HOURS)
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103 FINAL November 22 1968 o 136:00 - 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
CDR CMP LMP MCC—H 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
139:30 TORQUE ANGLES: (7 HOURS) (7 HOURS)
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
140:30 (7 HOURS) (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 •
141:00
141:15
FLIGHT PLAN CMP
I
LOSS OF COMM CONTINGENCY TRN BIAS [CISLUNAR NAVIGATION P23
1. STAR 22 EFH STAR E H 1 SET
2, STAR STAR
26 ENH E H
1 SET—
STAR 31 ENH STAR E H 1 SET —
LMP
BIOMED Sw - RIGHT'
MCC—H
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
CDR
MNVR TO SIGHTING ATT
TRN BIAS
ISLUNAR NAVIGATION P231
1. STAR 22 EFH STAR E H 1 SET
2. STAR 26 ENH STAR E H -- 1 SET
EAT PERIOD
•
FLIGHT PL AN CDR CMP LMP MCC-H
4 142:00
EAT PERIOD
142:15
142:3
142:45
I 143:00-1
LOSS OF COMM CONTINGENCY
•
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
CAW •
OAP CDR 143:00
MCC- Ii 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
EI-3 HRS
144:00
IMU REALIGN P52 OPTION 3 - REFSMMAT STAR ID STAR ANGLE RI F F-- —
TORQUE ANGLES7— -- X
CMC SELF CK DSKY COND LT TEST
ECS CK
EPS CK SPS CK SM/CM RCS CK C&W CK
•
MISSION EDITION DATE TIME DAY/REV
AS503/103 FINAL November 22, 1968 143:00 - 144:00 6/TEC
2 PAGE
-114 MSC Form 1910 (Nov 68) FLIGHT PLANNING BRANCH
BURN STATUS REPORT
■X
X --..+. ATIG
X X • • 1 T _
Ig x
, • W___1174
X X X IR
I P
1 Y !V gx
i V gy
IVgzF-1
AV C X X i ;FUEL
X X ; OX X X X , ;UNBALANCE
'REMARKS:
X X
X X
X
MCC'S
BURN CHART
P or Y RATES
ATT DEVIATION
SHUTDOWN TIME RESIDUALS .
MCC(ALL) 10°/SEC TAKEOVER
10° TAKEOVER
BIT +1 SEC TRIM TO 0.2 fps
0 0
0 ill I + 410
FLIGHT PLAN CMP
• MCC-H LMP 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
MCC 7 AV=NOMINALLY ZERO EI-2 HRS
MCC BURN STATUS REPORT V66 TRANS CSM STATE VECTOR TO LM SLOT
GDC ALIGN TO IMU
• .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
145: 00 —
EI-1.5 HR
145:30 —
E I -1 HR
146:00 —1
MNVR TO ENTRY ATT CCU STAR CK
GDC ALIGN TO IMU
FINAL STOWAGE
EMS CK
FINAL GDC DRIFT CK
BIOMED Sw - LEFT
FINAL STOWAGE
PIPA BIAS CK
LOSS OF COMM CONTINGENCY CISLUNAR NAVIGATION P23 1. STAR 33 ENH STARE H 1 SET -- --
SXT STAR CK
IMU REALIGN P52 OPTION 3 - REFSMMAT AND GYRO DRIFT TEST STAR ID , -- STAR ANGLE DIFF
TORQUE ANGLES: X Y
FINAL STOWAGE INITIATE CM RCS PREHEAT WASTE H 2 O DUMP - OFF
UR DUMP HT - OFF
FLIGHT PLAN CDR
CMP LMP
MCC-H
MISSION EDITION DATE TIME DAY/REV PAGE
AS503/103_ FINAL November 22, 196E 145:00 - 146:00 r
7/TEC 2-116 MSC form 1310 (Nov 68)
FLIGHT PLANNING BRANCH
• 0 • 4I■
0
146:00
EI-30 MIN
146:30
CDR •
SET DET TO EI EMS INITIALIZATION RSI ALIGN TO GDC CM RCS CK
SEPARATION CK LIST
MNVR TO CM/SM SEP ATT
FLIGHT PL AN CMP
TERM CM RCS PREHEAT
RECORD ENTRY PAD & RCVY INFO
SEPARATION CK LIST
P61 ENTRY PREP
LMP
PYRO BAT CK
ENTRY BATS - ON
SEPARATION CK LIST
GO FOR PYRO ARM
MCC—H I
P27 UPDATE: STATE VECTOR VOICE UPDATE: ENTRY PAD & RCVY INFO
GO FOR PYRO ARM
[CM/SM SEP EI-15 MIN
MNVR TO ENTRY ATT P62 ENTRY ATTITUDE
P63 ENTRY INITIATE
[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
146:50