Apollo 17 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 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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Terminal Countdown Sequencer (TCS) failed to issue the S-IVB LOX pressurization command. |
-000: |
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Unscheduled but automatic 1-hour 5-minute 11-second hold at T-30 seconds due to TCS failure. |
-000: |
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Countdown recycled to T-22 minutes. |
-000: |
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Unscheduled 1-hour 13-minute 19-second hold at T-8 minutes to resolve TCS corrective action. |
-000: |
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Countdown resumed at T-8 minutes. |
-000: |
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Guidance reference release. |
-000:00:16.960 |
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S-IC engine start command. |
-000:00:08.9 |
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S-IC engine ignition (#5). |
-000:00:06.9 |
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All S-IC engines thrust OK. |
-000:00:01.6 |
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Range zero. |
000:00:00.00 |
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All holddown arms released (1st motion) (1.08 g). |
000:00:00.24 |
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Liftoff (umbilical disconnected). |
000:00:00.63 |
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Tower clearance yaw maneuver started. |
000:00:01.7 |
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Yaw maneuver ended. |
000:00:09.7 |
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Pitch and roll maneuver started. |
000:00:12.9 |
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Roll maneuver ended. |
000:00:14.3 |
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Mach 1 achieved. |
000:01:07.5 |
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Maximum bending moment (96,000,000 lbf-in). |
000: |
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Maximum dynamic pressure (701.75 lb/ft2). |
000:01:22.5 |
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S-IC center engine cutoff command. |
000:02:19.30 |
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Pitch maneuver ended. |
000:02:40.1 |
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S-IC outboard engine cutoff. Maximum total inertial acceleration (3.87 g). |
000:02:41.20 |
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S-IC maximum Earth-fixed velocity. |
000:02:42.0 |
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S-IC/S-II separation command. |
000:02:42.9 |
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S-II engine start command. |
000:02:43.6 |
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S-II ignition. |
000:02:44.6 |
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S-II aft interstage jettisoned. |
000:03:12.9 |
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Launch escape tower jettisoned (planned time, actual time not recorded). |
000: |
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Iterative guidance mode initiated. |
000:03:24.1 |
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S-IC apex. |
000:04:33.689 |
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S-II center engine cutoff. Maximum total inertial acceleration (1.74 g). |
000:07:41.21 |
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S-IC impact (theoretical). |
000:09:11.708 |
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S-II outboard engine cutoff. |
000:09:19.66 |
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S-II/S-IVB separation command. S-II maximum Earth-fixed velocity. |
000:09:20.6 |
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S-IVB 1st burn start command. |
000:09:20.70 |
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S-IVB 1st burn ignition. |
000:09:23.80 |
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S-IVB ullage case jettisoned. |
000:09:32.4 |
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S-II apex. |
000:09:34.527 |
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S-IVB 1st burn cutoff and maximum total inertial acceleration (0.67 g). |
000:11:42.65 |
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Earth orbit insertion. |
000:11:52.65 |
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S-IVB 1st burn maximum Earth-fixed velocity. |
000:11:52.7 |
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Maneuver to local horizontal attitude started. |
000:12:04.4 |
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S-II impact (theoretical). |
000:19:56.947 |
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S-IVB 2nd burn restart preparation. |
003:02:58.60 |
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S-IVB 2nd burn restart command. |
003:12:28.60 |
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S-IVB 2nd burn ignition. |
003:12:36.60 |
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S-IVB 2nd burn cutoff and maximum total inertial acceleration (1.41 g). |
003:18:27.64 |
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S-IVB safing procedure – CVS opened. |
003:18:28.3 |
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S-IVB 2nd burn maximum Earth-fixed velocity. |
003:18:28.5 |
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Translunar injection. |
003:18:37.64 |
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Maneuver to local horizontal attitude and orbital navigation started. |
003:20:59.6 |
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Maneuver to transposition and docking attitude started. |
003:33:28.9 |
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CSM separated from S-IVB. |
003:42:27.6 |
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TV transmission started. |
003:50 |
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CSM docked with LM/S-IVB. |
003:57:10.7 |
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TV transmission ended. |
004:10 |
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CSM/LM ejected from S-IVB. |
004:45:02.3 |
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S-IVB APS evasive maneuver ignition. |
005:03:01.1 |
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S-IVB APS evasive maneuver cutoff (estimated). |
005:04:21.0 |
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S-IVB lunar impact maneuver - CVS opened. |
005:19:39.8 |
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S-IVB lunar impact maneuver - LOX dump started. |
005:24:20.2 |
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S-IVB lunar impact maneuver - CVS closed. |
005:24:40.0 |
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S-IVB lunar impact maneuver - LOX dump ended. |
005:25:07.9 |
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Maneuver to attitude for 1st S-IVB APS lunar impact burn. |
006: |
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S-IVB lunar impact maneuver - 1st APS ignition command. |
006:09:59.8 |
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S-IVB lunar impact maneuver - 1st APS cutoff command. |
006:11:38.0 |
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Maneuver to S-IVB solar heating attitude. |
006: |
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Maneuver to attitude for 2nd S-IVB APS lunar impact burn. |
011: |
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S-IVB lunar impact maneuver - 2nd APS ignition command. |
011:14:59.8 |
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S-IVB lunar impact maneuver - 2nd APS cutoff command. |
011:16:42.0 |
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S-IVB 3-axis tumble mode initiated. |
011:31:42 |
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S-IVB passive thermal control maneuver. |
011:31:50 |
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Command to inhibit instrument unit flight control computer to leave the S-IVB in 3-axis tumble mode. |
011:32:12.5 |
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Midcourse correction ignition (SPS). |
035:29:59.91 |
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Midcourse correction cutoff. |
035:30:01.64 |
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Maneuver to LM checkout attitude. |
039:05 |
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Preparations for intravehicular transfer. |
039:20 |
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LM pressurization started. |
039:30 |
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CDR and LMP entered LM for housekeeping and communications check. |
040:10 |
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LM closeout. |
042:11 |
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Heat flow and convection demonstration started. |
042:55 |
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Heat flow and convection demonstration ended. |
043:45 |
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Heat flow and convection demonstration started. |
045:20 |
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Heat flow and convection demonstration ended. |
046:00 |
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LM pressurization started. |
059:30 |
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CDR and LMP entered LM for telemetry checkout. |
059:59 |
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CDR and LMP entered CM. |
062:16 |
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065:00 |
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Apollo light flash phenomenon experiment started. |
065:39 |
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Apollo light flash phenomenon experiment ended. |
066:39 |
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Equigravisphere. |
070:37:45 |
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Scientific instrument module door jettisoned. |
081:32:40 |
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Inflight science phase of mission initiated with turn-on of Far Ultraviolet Spectrometer. |
083:26 |
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Ultraviolet photography of dark Moon. |
084:50 |
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Lunar orbit insertion ignition (SPS). |
086:14:22.60 |
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Lunar orbit insertion cutoff. |
086:20:55.76 |
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S-IVB impact on lunar surface. |
086:59:42.3 |
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Terminator photography. |
087:05 |
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Orbital science visual observations. |
087:15 |
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Orbital science photography. |
088:00 |
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1st descent orbit insertion ignition (SPS). |
090:31:37.43 |
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1st descent orbit insertion cutoff. |
090:31:59.70 |
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Landmark observations. |
090:50 |
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CDR and LMP entered LM. |
105:02 |
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CSM/LM separation maneuver initiated (RCS). |
107:47:56 |
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CSM/LM separation maneuver cutoff. |
107:47:59.4 |
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CSM orbit circularization ignition (SPS). |
109:17:28.92 |
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CSM orbit circularization cutoff. |
109:17:32.72 |
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2nd descent orbit insertion ignition (LM RCS). |
109:22:42 |
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2nd descent orbit insertion cutoff. |
109:23:03.5 |
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CSM landmark tracking started. |
109:40 |
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LM powered descent engine ignition (DPS). |
110:09:53 |
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LM throttle to full-throttle position. |
110:10:21 |
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LM manual target (landing site) update. |
110:11:25 |
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LM landing radar velocity data good. |
110:13:28 |
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LM landing radar range data good. |
110:14:06 |
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LM landing radar updates enabled. |
110:14:32 |
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LM throttle down. |
110:17:19 |
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LM approach phase program selected. |
110:19:15 |
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LM landing radar antenna to position 2. |
110:19:16 |
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LM 1st landing point redesignation. |
110:19:26 |
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LM landing radar switched to low scale. |
110:19:54 |
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LM landing phase program selected. |
110:20:51 |
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LM lunar landing and powered descent engine cutoff. |
110:21:58 |
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CSM landmark tracking ended. |
111:20 |
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1st EVA started (LM cabin depressurized). |
114:21:49 |
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CSM orbital science visual observations. |
114:45 |
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Lunar roving vehicle (LRV) offloaded. |
114:51:10 |
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LRV deployed, test drive performed and documented with photography, gathered samples and performed 500 mm and panoramic photography. |
115:13:50 |
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CSM orbital science photography. |
115:15 |
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115:40:58 |
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Traverse gravimeter experiment reading obtained. |
115:50:51 |
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Cosmic ray experiment deployed. |
115:54:40 |
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Apollo lunar surface experiment (ALSEP) package offloaded. |
115:58:30 |
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Traverse gravimeter experiment reading obtained. |
116:06:01 |
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Traverse gravimeter experiment reading obtained. |
116:11:54 |
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Traverse gravimeter experiment reading obtained. |
116:46:17 |
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CSM orbital science photography. |
117:10 |
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1st ALSEP data received on Earth. |
117: |
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Heat flow experiment turned on. |
117:29 |
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ALSEP deployment completed and documented with photographs and panoramic photography. |
118:07:43 |
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CSM terminator photography. |
118:10 |
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Lunar seismic profiling experiment (S-203) turned on. CSM Earthshine photography started. |
118:25 |
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Deep core sample obtained and lunar neutron probe experiment deployed. |
118:35:27 |
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