Apollo 9 Timeline
Event |
GET (hhh:mm:ss) |
GMT Time |
GMT Date |
Terminal countdown started. |
-028: |
|
|
Scheduled 3-hour hold at T-16 hours. |
-016: |
|
|
Decision made to recycle countdown to T-42 hours due to health of crew. |
-016: |
|
|
Countdown resumed at T-42 hours. |
-042: |
|
|
Scheduled 5-hour 30-minute hold at T-28 hours. |
-028: |
|
|
Countdown resumed at T-28 hours. |
-028: |
|
|
Scheduled 3-hour hold at T-16 hours. |
-016: |
|
|
Countdown resumed at T-16 hours. |
-016: |
|
|
Scheduled 6-hour hold at T-9 hours. |
-009: |
|
|
Countdown resumed at T-9 hours. |
-009: |
|
|
Guidance reference release. |
-000:00:16.97 |
|
|
S-IC engine start command. |
-000:00:08.9 |
|
|
S-IC engine ignition (#5). |
-000:00:06.3 |
|
|
All S-IC engines thrust OK. |
-000:00:01.3 |
|
|
Range zero. |
000:00:00.00 |
|
|
All holddown arms released (1st motion) (1.10 g). |
000:00:00.26 |
|
|
Liftoff (umbilical disconnected). |
000:00:00.67 |
|
|
Tower clearance yaw maneuver started. |
000:00:01.7 |
|
|
Yaw maneuver ended. |
000:00:09.7 |
|
|
Pitch and roll maneuver started. |
000:00:13.3 |
|
|
Roll maneuver ended. |
000:00:33.0 |
|
|
Mach 1 achieved. |
000:01:08.2 |
|
|
Maximum bending moment (86,000,000 lbf-in). |
000:01:19.4 |
|
|
Maximum dynamic pressure (630.73 lb/ft2). |
000:01:25.5 |
|
|
S-IC center engine cutoff command. |
000:02:14.34 |
|
|
Pitch maneuver ended. |
000:02:38.0 |
|
|
S-IC outboard engine cutoff. |
000:02:42.76 |
|
|
S-IC maximum total inertial acceleration (3.85 g). |
000:02:42.84 |
|
|
S-IC/S-II separation command and S-IC maximum Earth-fixed velocity. |
000:02:43.45 |
|
|
S-II engine start command. |
000:02:44.17 |
|
|
S-II ignition. |
000:02:45.16 |
|
|
S-II aft interstage jettisoned. |
000:03:13.5 |
|
|
Launch escape tower jettisoned. |
000:03:18.3 |
|
|
Iterative guidance mode initiated. |
000:03:24.6 |
|
|
S-IC apex. |
000:04:26.03 |
|
|
S-II engine cutoff. |
000:08:56.22 |
|
|
S-II maximum total inertial acceleration (2.00 g). |
000:08:56.31 |
|
|
S-IC impact (theoretical). |
000:08:56.436 |
|
|
S-II maximum Earth-fixed velocity. |
000:08:56.45 |
|
|
S-II/S-IVB separation command. |
000:08:57.18 |
|
|
S-IVB 1st burn start command. |
000:08:57.28 |
|
|
S-IVB 1st burn ignition. |
000:09:00.82 |
|
|
S-IVB ullage case jettisoned. |
000:09:09.0 |
|
|
S-II apex. |
000:09:53.58 |
|
|
S-IVB 1st burn cutoff. |
000:11:04.66 |
|
|
S-IVB 1st burn maximum total inertial acceleration (0.80 g). |
000:11:04.74 |
|
|
Earth orbit insertion. S-IVB 1st burn maximum Earth-fixed velocity. |
000:11:14.66 |
|
|
Maneuver to local horizontal attitude started. |
000:11:24.9 |
|
|
Orbital navigation started. |
000:12:47.7 |
|
|
S-II impact (theoretical). |
000:20:25.346 |
|
|
Maneuver to transposition and docking attitude.. |
002:34:01.0 |
|
|
CSM separated from S-IVB (command). |
002:41:16.0 |
|
|
Formation flying. CSM docked with LM/S-IVB. |
003:01:59.3 |
|
|
CSM/LM ejected from S-IVB. |
004: |
|
|
Maneuver to local horizontal attitude started. |
004:25:05.1 |
|
|
S-IVB 2nd burn restart preparation. |
004:36:17.24 |
|
|
S-IVB 2nd burn restart command. |
004:45:47.20 |
|
|
S-IVB 2nd burn ignition (for intermediate orbit insertion). |
004:45:55.54 |
|
|
S-IVB 2nd burn cutoff. |
004:46:57.60 |
|
|
S-IVB 2nd burn maximum total inertial acceleration (1.24 g). |
004:46:57.68 |
20:46:57 |
03 Mar 1969 |
S-IVB 2nd burn maximum Earth-fixed velocity. |
004:46:58.20 |
20:46:58 |
03 Mar 1969 |
S-IVB intermediate orbit insertion. |
004:47:07.60 |
20:47:07 |
03 Mar 1969 |
Orbital navigation started. |
004:47:14.2 |
20:47:14 |
03 Mar 1969 |
Maneuver to local horizontal attitude started. |
004:47:18.6 |
20:47:18 |
03 Mar 1969 |
1st SPS ignition. |
005:59:01.07 |
21:59:01 |
03 Mar 1969 |
1st SPS cutoff. |
005:59:06.30 |
21:59:06 |
03 Mar 1969 |
Powered flight navigation started. |
005:59:39.0 |
21:59:39 |
03 Mar 1969 |
S-IVB 3rd burn restart preparation. |
005:59:40.98 |
21:59:41 |
03 Mar 1969 |
S-IVB 3rd burn restart command. |
006:06:27.35 |
22:06:27 |
03 Mar 1969 |
S-IVB 3rd burn ignition (Earth escape trajectory). |
006:07:19.26 |
22:07:19 |
03 Mar 1969 |
S-IVB 3rd burn maximum total inertial acceleration (1.69 g). |
006:08:53.00 |
22:08:53 |
03 Mar 1969 |
S-IVB 3rd burn cutoff. |
006:11:21.32 |
22:11:21 |
03 Mar 1969 |
S-IVB safing procedures started. |
006:11:21.92 |
22:11:21 |
03 Mar 1969 |
S-IVB 3rd burn maximum Earth-fixed velocity. |
006:11:23.50 |
22:11:23 |
03 Mar 1969 |
S-IVB escape orbit insertion. |
006:11:31.32 |
22:11:31 |
03 Mar 1969 |
Orbital navigation started. |
006:11:38.0 |
22:11:38 |
03 Mar 1969 |
Maneuver to local horizontal attitude started. |
006:11:42.0 |
22:11:42 |
03 Mar 1969 |
S-IVB safing - LOX dump started (failed due to loss of engine pneumatic control during 3rd burn). |
006:12:15.5 |
22:12:15 |
03 Mar 1969 |
S-IVB safing - LOX NPV valve latched open to safe LOX tank |
006:24:02 |
22:24:02 |
03 Mar 1969 |
S-IVB safing - LH2 dump started (failed due to loss of pneumatic control of engine valves). |
006:24:11.3 |
22:24:11 |
03 Mar 1969 |
S-IVB safing - APS depletion firing ignition. |
007:34:04.6 |
|
|
S-IVB safing - APS depletion firing cutoff. |
007:41:53 |
|
|
2nd SPS ignition. |
022:12:04.07 |
|
|
2nd SPS cutoff. |
022:13:54.36 |
|
|
3rd SPS ignition. |
025:17:39.27 |
|
|
3rd SPS cutoff. |
025:22:19.15 |
|
|
4th SPS ignition. |
028:24:41.37 |
|
|
4th SPS cutoff. |
028:25:09.24 |
|
|
Pressure suits donned. |
041:00 |
|
|
LMP entered LM. |
043:15 |
|
|
LM transferred to internal power. |
043:40 |
|
|
LM systems activated. |
043:45 |
|
|
CDR entered LM. |
044:04 |
|
|
Landing gear deployed. |
045:00 |
|
|
Portable life support systems prepared. |
045:05 |
|
|
CDR requested private communication regarding LMP illness. |
045:39:05 |
|
|
CAPCOM replies that he is ready to receive CDR’s private communication. |
045:51:56 |
|
|
TV transmission (approximately 5 minutes). |
046:28 |
|
|
Self test of landing radar and rendezvous radar. |
048:15 |
|
|
DPS docked ignition. |
049:41:34.46 |
|
|
DPS docked cutoff. |
049:47:45.97 |
|
|
Landing radar self test. |
050:00 |
|
|
Transfer to CM started. |
050:15 |
|
|
LM deactivated. |
051:00 |
|
|
5th SPS ignition. |
054:26:12.27 |
|
|
5th SPS cutoff. |
054:26:55.53 |
|
|
Pressure suits removed. |
055:00 |
|
|
Pressure suits donned. |
068:15 |
|
|
Transfer to LM started. |
069:45 |
|
|
LM systems activated. |
070:00 |
|
|
CDR assessed LMP condition as excellent. |
071:53 |
|
|
LM depressurized. |
072:45 |
|
|
LM forward hatch open. |
072:46 |
|
|
CM depressurized. |
072:59 |
16:59 |
|
LMP started egress. |
072:59:02 |
|
|
CM side hatch open. |
073: |
|
|
CDR reported LMP’s foot extending through LM forward hatch. LMP lowered EVA visor. |
073:04 |
|
|
LMP egress completed. Entered foot restraints. CDR photographed LMP activities. |
073:07 |
|
|
CDR passed 70 mm camera to LMP. LMP started photography. |
073:10 |
|
|
LMP ended 70 mm photography and handed camera to CDR.CMP photographed LM with 16 mm camera. |
073:20 |
|
|
CDR passed 16 mm camera to LMP. CMP activities photographed by LMP. |
073:23 |
|
|
CMP retrieved SM thermal samples. |
073:26 |
|
|
LMP passed 16 mm camera to CDR. |
073:34 |
|
|
LMP 16 mm camera failed. LMP evaluated handrail, retrieved LM thermal sample, and passed to CDR. |
073:39 |
|
|
LMP started handrail evaluation. |
073:42 |
|
|
LMP ingress started. |
073:45 |
|
|
LMP ingress completed. |
073:46:03 |
|
|
LM hatch closed. |
073:48 |
|
|
CM side hatch reported closed and locked. |
073:49:23 |
|
|
LM hatch reported locked. |
073:49:56 |
|
|
LM repressurized at 3.0 psi. |
073:53 |
|
|
CM repressurization started. |
073:55 |
|
|
CM repressurized at 2.7 psi. |
074: |
|
|
TV transmission started. |
074:58:03 |
|
|
TV transmission ended. |
075:13:13 |
|
|
CDR entered CM. |
075:15 |
|
|
LMP entered CM. |
076:55 |
|
|
Pressure suits removed. |
077:15 |
|
|
LMP entered LM to open translunar bus tie circuit breakers. |
078:09 |
|
|
Pressure suits donned. |
086:00 |
|
|
LMP entered LM. |
088:05 |
|
|
LM systems activated. |
088:15 |
|
|
CDR entered LM. |
088:55 |
|
|
Check LM systems. |
089:05 |
|
|
Rendezvous radar transponder test. |
091:00 |
|
|
Landing radar self test. |
091:55 |
|
|
Rendezvous radar transponder test. |
092:05 |
|
|
Maneuver to undocking attitude. |
092:22 |
|
|
Unsuccessful undocking attempt. Capture latches failed to release. |
092:38 |
|
|
CSM/LM reported undocked. |
092:39:36 |
|
|
Formation flying and photography. |
092:45 |
|
|
CSM/LM separation maneuver ignition. |
093:02:54 |
|
|
CSM/LM separation maneuver cutoff. |
093:03:03.5 |
|
|
LM descent propulsion phasing maneuver ignition. |
093:47:35.4 |
|
|
LM descent propulsion phasing maneuver cutoff. |
093:47:54.4 |
|
|
Landing radar self test. |
094:15 |
|
|
Rendezvous radar on. |
095:10 |
|
|
LM descent propulsion insertion maneuver ignition. |
095:39:08.06 |
|
|
LM descent propulsion insertion maneuver cutoff. |
095:39:30.43 |
|
|
CAPCOM reported “everything looks good for staging.” |
095:58:15 |
|
|
LM coelliptic sequence initiation maneuver ignition. Approximate time of LM descent stage jettison. |
096:16:06.54 |
|
|
LM coelliptic sequence initiation maneuver cutoff. |
096:16:38.25 |
|
|
CDR reports LM “staging went okay.” |
096:33:11 |
|
|
LM constant differential height ignition. |
096:58:15.0 |
|
|
LM constant differential height cutoff. |
096:58:17.9 |
|
|
LM terminal phase initiation ignition. |
097:57:59 |
|
|
LM terminal phase initiation cutoff. |
097:58:36.6 |
|
|
1st RCS midcourse correction ignition. |
098:25:19.66 |
|
|
1st RCS midcourse correction cutoff. |
098:25:23.57 |
|
|
Terminal phase braking. |
098:30:03 |
|
|
Stationkeeping. |
098:30:51.2 |
|
|
Formation flying and photography. |
098:40 |
|
|
CSM/LM docked. |
099:02:26 |
|
|
CDR entered CM. |
100:35 |
|
|
LM prepared for jettison. |
100:40 |
|
|
LMP entered CM. |
101:00 |
|
|
LM ascent stage jettisoned. |
101:22:45.0 |
|
|
Post-jettison CSM separation maneuver. |
101:32:44 |
|
|
LM ascent engine depletion ignition. |
101:53:15.4 |
|
|
LM ascent engine depletion. |
101:59:17.7 |
|
|
Pressure suits removed. |
102:00 |
|
|
6th SPS ignition. |
123:25:06.97 |
|
|
6th SPS cutoff. |
123:25:08.40 |
|
|
Experiment S065 photography. |
124:10 |
|
|
CSM landmark tracking. |
125:30 |
|
|
CSM landmark tracking. |
143:00 |
|
|
Experiment S065 photography. |
146:00 |
|
|
Experiment S065 photography. |
147:30 |
|
|
Target of opportunity photography. |
149:00 |
|
|
Target of opportunity photography. |
150:10 |
|
|
7th SPS ignition. |
169:39:00.36 |
|
|
7th SPS cutoff. |
169:39:25.26 |
|
|
16 mm photography. |
171:10 |
|
|
Experiment S065 photography. |
171:20 |
|
|
Experiment S065 photography. |
171:50 |
|
|
Target of opportunity photography. |
173:10 |
|
|
Experiment S065 photography. |
190:40 |
|
|
Experiment S065 photography. |
192:10 |
|
|
Tracking of Pegasus II satellite started. |
192:43 |
|
|
Tracking of Pegasus II satellite ended. |
192:44 |
|
|
High-gain antenna test. |
193:10 |
|
|
High-gain antenna test. |
193:40 |
|
|
Target of opportunity photography. |
193:50 |
|
|
Tracking of Pegasus II satellite started. |
194:13 |
|
|
Tracking of Pegasus II satellite ended. |
194:15 |
|
|
CSM landmark tracking. |
195:10 |
|
|
Target of opportunity photography. |
195:30 |
|
|
Target of opportunity photography. |
213:25 |
|
|
Observation of descent stage attempted. |
213:50 |
|
|
Target of opportunity photography. |
215:00 |
|
|
Experiment S065 photography. |
215:10 |
|
|
Target of opportunity photography. |
215:30 |
|
|
Experiment S065 photography. |
216:10 |
|
|
Target of opportunity photography. |
216:20 |
|
|
Experiment S065 photography. |
216:40 |
|
|
Target of opportunity photography. |
217:00 |
|
|
CSM landmark tracking. |
217:50 |
|
|
Passive thermal control evaluated. |
218:30 |
|
|
Passive thermal control evaluated. |
222:00 |
|
|
Tracking of ascent stage with optics started. |
222:38:40 |
|
|
Tracking of ascent stage with optics ended. |
222:45:40 |
|
|
8th SPS ignition (deorbit). |
240:31:14.84 |
|
|
8th SPS cutoff. |
240:31:26.58 |
|
|
CM/SM separation. |
240:36:03.8 |
|
|
Entry. |
240:44:10.2 |
|
|
Communication blackout started. |
240:47:01 |
|
|
Communication blackout ended. |
240:50:43 |
|
|
Radar contact with CM established by recovery aircraft. |
240:51 |
|
|
Drogue parachute deployed |
240:55:07.8 |
|
|
Main parachute deployed. |
240:55:59.0 |
|
|
Recovery beacon contact with CM established by recovery aircraft. VHF voice contact with CM established by recovery helicopter. |
240:57 |
|
|
Visual contact with CM established by recovery helicopter. |
240:58 |
|
|
Splashdown (went to apex-up). |
241:00:54 |
|
|
Swimmers and flotation collar deployed. |
241:07 |
|
|
Flotation collar inflated. |
241:14 |
|
|
CM hatch opened. |
241:27 |
|
|
Crew aboard recovery helicopter. |
241:45 |
|
|
Crew aboard recovery ship. |
241:49:33 |
|
|
CM aboard recovery ship. |
243:13 |
|
|
Crew departed recovery ship. |
263:00 |
|
|
Crew arrived in Eleuthera in the |
264:30 |
|
|
Deactivation of CM started at Norfolk Naval Air Station, VA. |
312:00 |
|
|
CM arrived at contractor’s facility in |
|
|
|
LM descent stage entry. |
443:45 |
|
|
LM ascent stage entry. |
|
|
|