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Apollo 15

CSM Guidance & Control Checklist - Index

• Frontispiece
• Introduction
• i List of effective pages
• ii List of effective pages (continued)
• iia List of effective pages (continued)
• iii Contents
• iv Contents (continued)
• v Contents (continued)
• vi Contents (continued)

CMC General

• 1-01 Star list
• 1-02 Verb list
• 1-03 Verb list (continued)
• 1-04 Noun list (Decimal)
• 1-05 Noun list (Decimal) (continued)
• 1-06 Noun list (Decimal) (continued)
• 1-07 Noun list (Decimal) (continued)
• 1-08 Noun list (Decimal) (continued), Verb 05 Noun 09 alarm codes
• 1-09 Verb 05 Noun 09 alarm codes (continued)
• 1-10 Verb 05 Noun 09 alarm codes (continued)
• 1-11 Verb 05 Noun 09 alarm codes (continued)
• 1-12 Verb 05 Noun 09 alarm codes (continued)
• 1-13 Verb 05 Noun 09 alarm codes (continued)
• 1-14 Verb 50 Noun 25 checklist codes, Verb 04 Noun 06 (Noun 12) option codes
• 1-15 Flag word listing
• 1-16 Flag word listing (continued)
• 1-17 Flag word listing (continued)
• 1-18 Octal-to-binary conversion
• 1-19 Chart - CMC input/output channels
• 1-20 Flag word & channel set/reset
• 1-21 Octal-to-decimal conversion - Review data in erasable memory - To change data in erasable memory - Monitor of input/output channels
• 1-22 RCS DAP attitude deadband change - VHF range DSKY display
• 1-23 G&N recovery procedures
• 1-24 General system checkout
• 1-25 Verb 35-DSKY condition light test - Verb 41 Noun 91 coarse align OCDUs
• 1-26 Verb 41 Noun 91 coarse align OCDUs (continued) - Verb 41 Noun 20 coarse align ICDUs - Verb 42 gyro torquing
• 1-27 Verb 48-DAP data load & activate procedure
• 1-28 Verb 49 Crew defined maneuver - Verb 55 CMC time update - Verb 64 Hi Gain Antenna pointing
• 1-29 Verb 67 W-matrix error display - Verb 74 CMC downlink - Verb 79 DAP PTC/orb rate
• 1-30 Verb 82 Orbit parameter display
• 1-31 Verb 83 Rendezvous parameter display #1 - Verb 85 rendezvous parameter display #2 - Verb 87 set VHF range flag
• 1-32 Verb 89 Rendezvous final attitude
• 1-33 Verb 90 Out-of-plane display - Verb 91 compute banksum - Verb 93 Enable W-matrix initialisation

G&C system management

• 2-01 IMU power up procedure, IMU power down procedure
• 2-02 Measurement & loading of PIPA bias - CMC power up procedure - Program 06 CMC power down procedure
• 2-03 CMC self check - Optics power up procedure - Optics power down - Scanning telescope manual drive procedure
• 2-04 SCS power up - SCS power down
• 2-05 SCS attitude reference comparison - EMS delta-V test & null bias check

Navigation (P20s)

• 3-01 Program 20 Rendezvous navigation
• 3-02 Program 20 (continued)
• 3-03 Program 21 Ground track determination
• 3-04 Program 22 Orbital navigation
• 3-05 Program 22 (continued)
• 3-06 Program 23 Cislunar midcourse nav measurement
• 3-07 Program 23 (continued)
• 3-08 Program 23 (continued)
• 3-09 Program 23 (continued)
• 3-10 Program 24 Rate-aided optics tracking
• 3-11 Program 27 CMC update
• 3-12 Program 20 with GDC REFSMMAT
• 3-13 Program 20 (continued)

Prethrust (P30s & P70s)

• 4-01 Program 30 External delta-V - Program 32 CSI prethrust (P72 in LM)
• 4-02 Program 32 (continued)
• 4-03 Program 33 CDH prethrust (P73 in LM)
• 4-04 Program 34 TPI prethrust (P74 in LM)
• 4-05 Program 34 (continued)
• 4-06 Program 35 TPM prethrust (P75 in LM)
• 4-07 Program 37 Return to Earth program
• 4-08 Program 37 (continued)
• 4-09 Program 37 (continued)
• 4-10 Program 37 Return to Earth program (continued)
• 4-11 Chart, Delta-V required for Return to Earth (P37), K = 0.04 to 0.004
• 4-12 Chart, Delta-V required for Return to Earth (P37), K = 0.4 to 0.04
• 4-13 Program 37 Block data PAD form
• 4-14 Program 37 Block data PAD form
• 4-15 Program 76 Target delta-V

Thrusting (P40s)

• 5-01 Program 40 SPS thrusting
• 5-02 Program 40 (continued)
• 5-03 Program 40 (continued)
• 5-04 Program 40 (continued)
• 5-05 Program 40 (continued)
• 5-06 Program 40 (continued)
• 5-07 Program 40 (continued)
• 5-08 Chart, Propellant consumption chart, 3-axis attitude maneuvers
• 5-09 Chart, Propellant consumption chart, X-translation maneuvers
• 5-10 Chart, SPS versus RCS chart (2-jet ullage, CSM only)
• 5-11 Chart, SPS versus RCS chart (2-jet ullage, CSM/LM docked)
• 5-12 Chart, SPS versus RCS chart (4-jet ullage, CSM only)
• 5-13 Chart, SPS versus RCS chart (4-jet ullage, CSM/LM docked)
• 5-14 Chart, SPS engine trim gimbal angles versus spacecraft weight (CSM only)
• 5-15 Chart, SPS engine trim gimbal angles versus spacecraft weight (CSM/LM docked)
• 5-16 Program 41 RCS thrusting
• 5-17 Program 41 RCS thrusting
• 5-18 Program 41 (continued)
• 5-19 Program 41 (continued) - Program 47 Thrust monitor program

Alignments (P50s)

• 6-01 Program 51 IMU orientation
• 6-02 Program 52 IMU realignment
• 6-03 Program 52 (continued)
• 6-04 Program 52 (continued) - Program 53 backup IMU orient determination
• 6-05 Program 53 (continued) - Program 54 backup IMU realignment
• 6-06 Program 54 (continued)
• 6-07 Program 54 (continued)
• 6-08 Polar star maps
• 6-09 Equatorial star map
• 6-10 Equatorial star map

Initialisation procedures

• 7-01 Rapid IMU realignment - Changing landing site REFSMMAT for out-of-plane burns
• 7-02 Changing landing site REFSMMAT for out-of-plane burns (continued)
• 7-03 GDC alignment to IMU gimbal angles - Backup GDC and/or IMU alignment
• 7-04 In-plane GDC alignment
• 7-05 PGNS ORDEAL initialisation - SCS ORDEAL initialisation
• 7-06 COAS LOS determination
• 7-07 CMC/LGC clock sync/T_ephem update - Verb 55 CMC time update - Align LM IMU to CSM IMU
• 7-08 Align LM IMU to CSM GDC - Align LM AGS to CSM IMU/GDC
• 7-09 Align CSM GDC to LM IMU - Align CSM GDC to LM AGS
• 7-10 Align CSM IMU to LM IMU
• 7-11 Align CSM IMU to LM AGS - Crescent align
• 7-12 Crescent align (continued)
• 7-13 GDC REFSMMAT determination
• 7-14 GDC REFSMMAT determination (continued) - GDC REFSMMAT realignment (P52)
• 7-15 GDC REFSMMAT realignment (P52) (continued)
• 7-16 GDC REFSMMAT realignment (P52) (continued)
• 7-17 LM steerable antenna pointing

PTC/orb-rate procedures

• 8-01 Program 20 - (PTC/orb-rate)
• 8-02 Passive Thermal Control (G&N)
• 8-03 Passive Thermal Control (SCS)
• 8-04 Terminate PTC - Pitch orbit rate maneuver (G&N)
• 8-05 Pitch orbit rate maneuver (SCS)

Erasable load update

• 9-01 Erasable load update
• 9-02 To check state vector
• 9-03 Blank page
• 9-04 Register contents
• 9-05 Register contents
• 9-06 Register contents
• 9-07 Register contents)
• 9-08 LM or CSM state vector read-out and loading

Planet vectors

• 10-01 Venus unit vectors
• 10-02 Venus unit vectors (continued)
• 10-03 Mars, Jupiter and Saturn unit vectors

Copyright © 2016 by W. David Woods. All rights reserved.

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