Apollo 15 Timeline
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Event |
GET (hhh:mm:ss) |
GMT Time |
GMT Date |
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Terminal countdown started. |
-028: |
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Scheduled 9-hour 34-minute hold at T-9 hours. |
-009: |
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Countdown resumed at T-9 hours. |
-009: |
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Scheduled 1-hour hold at T-3 hours 30 minutes. |
-003:30:00 |
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Countdown resumed at T-3 hours 30 minutes. |
-003:30:00 |
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Guidance reference release. |
-000:00:16.939 |
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S-IC engine start command. |
-000:00:08.9 |
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S-IC engine ignition (#5). |
-000:00:06.50 |
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All S-IC engines thrust OK. |
-000:00:01.4 |
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Range zero. |
000:00:00.00 |
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All holddown arms released (1st motion) (1.08 g). |
000:00:00.3 |
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Liftoff (umbilical disconnected). |
000:00:00.58 |
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Tower clearance yaw maneuver started. |
000:00:01.68 |
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Yaw maneuver ended. |
000:00:09.66 |
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Pitch and roll maneuver started. |
000:00:12.21 |
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Roll maneuver ended. |
000:00:23.02 |
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Mach 1 achieved. |
000:01:05.0 |
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Maximum bending moment (80,000,000 lbf-in). |
000:01:20.1 |
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Maximum dynamic pressure (768.58 lb/ft2). |
000:01:22.0 |
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S-IC center engine cutoff command. |
000:02:15.96 |
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Pitch maneuver ended. |
000:02:36.94 |
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S-IC outboard engine cutoff. Maximum total inertial acceleration (3.97 g). |
000:02:39.56 |
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S-IC maximum Earth-fixed velocity. |
000:02:40.00 |
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S-IC/S-II separation command. |
000:02:41.2 |
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S-II engine start command. |
000:02:41.9 |
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S-II ignition. |
000:02:43.0 |
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S-II aft interstage jettisoned. |
000:03:11.2 |
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Launch escape tower jettisoned. |
000:03:15.9 |
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Iterative guidance mode initiated. |
000:03:22.62 |
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S-IC apex. |
000:04:37.562 |
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S-II maximum total inertial acceleration (1.79 g). S-II center engine cutoff. |
000:07:39.56 |
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S-II outboard engine cutoff. |
000:09:09.06 |
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S-II maximum Earth-fixed velocity. |
000:09:10.00 |
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S-II/S-IVB separation command. |
000:09:10.1 |
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S-IVB 1st burn start command. |
000:09:10.20 |
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S-IVB 1st burn ignition. |
000:09:13.20 |
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S-II apex. |
000:09:13.225 |
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S-IC impact (theoretical). |
000:09:20.839 |
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S-IVB ullage case jettisoned. |
000:09:21.8 |
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S-IVB 1st burn maximum total inertial acceleration (0.65 g). S-IVB 1st burn cutoff. |
000:11:34.67 |
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Earth orbit insertion. S-IVB 1st burn maximum Earth-fixed velocity. |
000:11:44.67 |
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Orbital navigation started. |
000:11:56.3 |
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Maneuver to local horizontal attitude started. |
000:13:15.7 |
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S-II impact (theoretical). |
000:19:43.912 |
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S-IVB 2nd burn restart preparation. |
002:40:24.80 |
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S-IVB 2nd burn restart command. |
002:49:54.90 |
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S-IVB 2nd burn ignition. |
002:50:02.90 |
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S-IVB 2nd burn cutoff and maximum total inertial acceleration (1.40 g). |
002:55:53.61 |
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S-IVB 2nd burn maximum Earth-fixed velocity. |
002:55:54.00 |
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Translunar injection. |
002:56:03.61 |
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Orbital navigation started. |
002:58:26.0 |
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Maneuver to local horizontal attitude started. |
002:58:26.2 |
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Maneuver to transposition and docking attitude started. |
003:10:54.6 |
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CSM separated from S-IVB. |
003:22:27.2 |
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TV transmission started. |
003:25 |
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CSM docked with LM/S-IVB. |
003:33:49.5 |
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TV transmission ended. |
003:50 |
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CSM/LM ejected from S-IVB. |
004:18:01.2 |
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S-IVB APS evasive maneuver ignition. |
004:40:01.8 |
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S-IVB APS evasive maneuver cutoff. |
004:41:22.0 |
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Maneuver to S-IVB LOX dump attitude initiated. |
004:49:41.8 |
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S-IVB lunar impact maneuver - CVS venting closed. |
004:56:40.6 |
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S-IVB lunar impact maneuver - LOX dump. Start of unplanned velocity increment due to J-2 engine control helium dump. |
005:01:20.6 |
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S-IVB lunar impact maneuver - CVS vent opened. |
005:01:40.6 |
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S-IVB lunar impact maneuver - LOX dump ended. |
005:02:08.7 |
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S-IVB lunar impact maneuver - J-2 engine control helium dump ended. |
005: |
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Maneuver to attitude required for final S-IVB APS burn initiated. |
005:27:13.5 |
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S-IVB lunar impact maneuver - 1st APS ignition. |
005:46:00.7 |
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S-IVB lunar impact maneuver - 1st APS cutoff. |
005:52:01.9 |
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S-IVB lunar impact maneuver - Start of 1st unplanned velocity increment due to instrument unit thermal control system water valve operations and APS attitude engine reactions. |
006: |
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S-IVB lunar impact maneuver - End of 1st velocity increment due to IU/TCS and APS effects. |
006: |
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S-IVB lunar impact maneuver - Start of 2nd velocity increment due to IU/TCS and APS effects. |
006:58:00 |
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S-IVB lunar impact maneuver - End of 2nd velocity increment due to IU/TCS and APS effects. |
007: |
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S-IVB lunar impact maneuver - Start of 3rd velocity increment due to IU/TCS and APS effects. |
007:38:00 |
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S-IVB lunar impact maneuver - End of 3rd velocity increment due to IU/TCS and APS effects. |
007:43:00 |
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S-IVB lunar impact maneuver - Start of 4th velocity increment due to IU/TCS and APS effects. |
008: |
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S-IVB lunar impact maneuver - End of 4th velocity increment due to IU/TCS and APS effects. |
008: |
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S-IVB lunar impact maneuver - Start of 5th velocity increment due to IU/TCS and APS effects. |
008:53:00 |
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S-IVB lunar impact maneuver - End of 5th velocity increment due to IU/TCS and APS effects. |
008:58:00 |
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S-IVB lunar impact maneuver - Start of 6th velocity increment due to IU/TCS and APS effects. |
009:28:00 |
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S-IVB lunar impact maneuver - End of 6th velocity increment due to IU/TCS and APS effects. |
009:33:00 |
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S-IVB lunar impact maneuver - 2nd APS ignition. |
010: |
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S-IVB lunar impact maneuver - 2nd APS cutoff. |
010: |
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S-IVB 0.3° per second solar heating avoidance roll command. |
010: |
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Midcourse correction ignition. |
028:40:22.0 |
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Midcourse correction cutoff. |
028:40:22.8 |
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Sextant photography test started. |
032:00 |
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Sextant photography test ended. |
032:50 |
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Preparations for LM ingress. |
033:25 |
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CDR and LMP entered LM for checkout. |
033:56 |
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TV transmission of CM and LM interiors started. |
034:55 |
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TV transmission of CM and LM interiors ended. |
035:46 |
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CDR and LMP entered CM. |
036:55 |
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Visual light flash phenomenon observations started. |
051:37 |
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Visual light flash phenomenon observations ended. |
052:33 |
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LM housekeeping. |
056:26 |
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LM ingress and housekeeping. |
056:26 |
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CDR and LMP entered LM for checkout. |
057:00 |
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CDR and LMP entered CM. |
058:00 |
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Equigravisphere. |
063:55:20 |
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Midcourse correction ignition. |
073:31:14.81 |
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Midcourse correction cutoff. |
073:31:15.72 |
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Scientific instrument module door jettisoned. |
074:06:47.1 |
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Lunar orbit insertion ignition (SPS). |
078:31:46.70 |
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Lunar orbit insertion cutoff. |
078:38:25.06 |
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S-IVB impact on lunar surface. |
079:24:42.9 |
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Orbital science photography started. |
080:35 |
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Orbital science photography ended. |
080:50 |
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Terminator photography. |
082:00 |
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Descent orbit insertion ignition (SPS). |
082:39:49.09 |
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Descent orbit insertion cutoff. |
082:40:13.62 |
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CSM landmark tracking. |
083:45 |
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Terminator photography. |
084:35 |
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TV transmission of landing site started. |
095:00 |
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TV transmission of landing site ended. |
095:10 |
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Descent orbit trim ignition (RCS). |
095:56:44.70 |
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Descent orbit trim cutoff. |
095:57:15.10 |
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CDR and LMP entered LM for activation, checkout, and platform alignment. |
098:00 |
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CM/LM undocking failure due to loose CM/LM umbilical. |
100:14 |
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LM undocking and separation. |
100:39:16.2 |
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CSM orbit circularization ignition (SPS). |
101:38:58.98 |
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CSM orbit circularization cutoff. |
101:39:02.65 |
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CSM lunar surface landmark tracking. |
102:35 |
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LM landing radar on. |
104:25:13.0 |
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LM powered descent engine ignition. |
104:30:09.4 |
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LM throttle to full-throttle position. |
104:30:35.9 |
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LM manual target (landing site) update. |
104:31:44.2 |
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LM pitchover started. |
104:33:10.4 |
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LM landing radar range data good. |
104:33:26.2 |
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LM landing radar altitude data good. |
104:33:38.2 |
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LM landing radar updates enabled. |
104:33:50.2 |
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LM throttle down. |
104:37:31.1 |
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LM approach phase program selected. |
104:39:32.2 |
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LM landing radar antenna to position 2. |
104:39:39.0 |
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LM 1st landing point redesignation. |
104:39:40.0 |
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LM landing radar switched to low scale. |
104:40:13.0 |
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LM attitude hold mode selected. |
104:41:08.7 |
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LM landing phase program selected. |
104:41:10.2 |
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LM powered descent engine cutoff. |
104:42:28.6 |
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LM lunar landing (right side and forward footpad contact). |
104:42:29.3 |
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LM final settling. |
104:42:31.1 |
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CSM orbital science photography. |
106:00 |
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Stand-up EVA started (Scott). |
106:42:49 |
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Stand-up EVA ended. |
107:15:56 |
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CSM orbital science photography. |
108:00 |
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CSM orbital science photography. |
108:40 |
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CSM bistatic radar test. |
110:00 |
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1st EVA started (LM cabin depressurized). |
119:39:17 |
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TV transmission started for 1st EVA. |
119:52:45 |
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Contingency sample collected. |
120:00:05 |
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Lunar rover vehicle (LRV) offloaded. |
120:18:31 |
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LRV deployed. |
120:31:33 |
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LRV configured for traverse. |
121:24:03 |
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Departed for station 1. |
121:44:55 |
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Arrived at station 1. Performed radial sampling, gathered documented samples, and performed panoramic photography. |
122:10:46 |
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Departed for station 2. |
122:22:36 |
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Arrived at station 2. Gathered samples, obtained a double core tube sample and performed stereopanoramic and 500 mm photography. |
122:34:44 |
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CSM deep space measurements. |
122:40 |
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CSM sunrise solar corona photography. |
123:05 |
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Departed for LM. |
123:26:02 |
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Arrived at LM. Offloaded and deployed Apollo lunar surface experiment package (ALSEP), laser ranging retroreflector, and solar wind composition experiment. |
123:59:39 |
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CSM sunset solar corona photography. |
124:30 |
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CSM lunar libration photography. |
125:00 |
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1st ALSEP data received on Earth. |
125: |
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TV transmission ended for 1st EVA. |
125:55 |
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Cold cathode gage experiment turned on. CSM orbital science photography. |
126:00 |
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1st EVA ended (cabin repressurized). |
126:11:59 |
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