| Time
(UTC/GMT+0) | | Event |
|
|
| 1968-10-12 | | Individual and combined CM and SM systems test completed at factory. |
|
| 1968-10-21 | | LM #5 integrated test at factory. |
|
| 1968-12-06 | | Integrated CM and SM systems test completed at factory. |
|
| 1968-12-13 | | LM #5 final engineering evaluation acceptance test at factory. |
|
| 1969-01-07 | | LM ascent stage #5 ready to ship from factory to KSC. |
|
| 1969-01-08 | | LM ascent stage #5 delivered to KSC. |
|
| 1969-01-10 | | Spacecraft/LM adapter #14 delivered to KSC. |
|
| 1969-01-11 | | LM descent stage #5 ready to ship from factory to KSC. |
|
| 1969-01-12 | | LM descent stage #5 delivered to KSC. |
|
| 1969-01-15 | | CSM #107 quads delivered to KSC. |
|
| 1969-01-18 | | Saturn S-IVB stage #506 delivered to KSC. |
|
| 1969-01-19 | | Saturn S-IVB stage #506 delivered to KSC. |
|
| 1969-01-22 | | CM #107 and SM #107 ready to ship from factory to KSC. |
|
| 1969-01-23 | | CM #107 and SM #107 delivered to KSC. |
|
| 1969-01-29 | | CM #107 and SM #107 mated. |
|
| 1969-02-06 | | Saturn S-II stage #6 delivered to KSC. |
|
| 1969-02-14 | | LM ascent stage #5 and descent stage #5 mated. |
|
| 1969-02-17 | | CSM #107 combined systems test completed. |
|
| 1969-02-17 | | LM #5 combined systems test completed. |
|
| 1969-02-20 | | Saturn S-IC stage #6 delivered to KSC. |
|
| 1969-02-21 | | Saturn S-IC stage #6 erected. |
|
| 1969-02-27 | | Saturn V instrument unit #506 delivered to KSC. |
|
| 1969-03-04 | | Saturn S-II stage #6 erected. |
|
| 1969-03-05 | | Saturn S-IVB stage #506 erected. |
|
| 1969-03-05 | | Saturn V instrument unit #506 erected. |
|
| 1969-03-18 | | CSM #107 altitude test with prime crew completed. |
|
| 1969-03-21 | | LM #5 altitude test with prime crew completed. |
|
| 1969-03-24 | | CSM #107 altitude tests completed. |
|
| 1969-03-25 | | LM #5 altitude tests completed. |
|
| 1969-03-27 | | Launch vehicle propellant dispersion/malfunction overall test completed. |
|
| 1969-04-14 | | CSM #107 moved to VAB |
|
| 1969-04-14 | | Spacecraft erected. |
|
| 1969-04-18 | | LM #5 combined systems test completed. |
|
| 1969-04-22 | | CSM #107 integrated systems test completed. |
|
| 1969-05-05 | | CSM #107 electrically mated to launch vehicle. |
|
| 1969-05-06 | | Space vehicle overall test completed. |
|
| 1969-05-14 | | Space vehicle overall test #1 (plugs in) completed. |
|
| 1969-05-20 | | Space vehicle and MLP #1 transferred to launch complex 39A. |
|
| 1969-05-22 | | Mobile service structure transferred to launch complex 39A. |
|
| 1969-06-02 | | LM #4 flight readiness test completed. |
|
| 1969-06-06 | | Space vehicle flight readiness test completed. |
|
| 1969-06-25 | | Saturn S-IC stage #6 RP-1 fuel loading completed. |
|
| 1969-07-02 | | Space vehicle countdown demonstration test (wet) completed. |
|
| 1969-07-03 | | Space vehicle countdown demonstration test (dry) completed. |
|
| 1969-07-14 21:00:00 | | Terminal countdown started. |
|
| 1969-07-15 16:00:00 | | Scheduled 11-hour hold at T-9 hours. |
|
| 1969-07-16 03:00:00 | | Countdown resumed at T-9 hours. |
|
| 1969-07-16 08:30:00 | | Scheduled 1-hour 32-minute hold at T-3 hours 30 minutes. |
|
| 1969-07-16 10:02:00 | | Countdown resumed at T-3 hours 30 minutes. |
|
| 1969-07-16 13:31:43 | | Guidance reference release. |
|
| 1969-07-16 13:31:51 | | S-IC engine start command. |
|
| 1969-07-16 13:31:53 | | S-IC engine ignition (#5). |
|
| 1969-07-16 13:31:58 | | All S-IC engines thrust OK. |
|
| 1969-07-16 13:32:00 | | Range zero. |
|
| 1969-07-16 13:32:00 | | All holddown arms released (1st motion). |
|
| 1969-07-16 13:32:00 | | Liftoff (umbilical disconnected) (1.07 g). |
|
| 1969-07-16 13:32:01 | | Tower clearance yaw maneuver started. |
|
| 1969-07-16 13:32:09 | | Yaw maneuver ended. |
|
| 1969-07-16 13:32:13 | | Pitch and roll maneuver started. |
|
| 1969-07-16 13:32:31 | | Roll maneuver ended. |
|
| 1969-07-16 13:33:06 | | Mach 1 achieved. Altitude 4.236nm. Downrange 1.044nm. Speed 1054ft/sec. |
|
| 1969-07-16 13:33:23 | | Maximum dynamic pressure (735.17 lb/ft2). Altitude 7.326nm. Downrange 3.012nm. Speed 1653ft/sec. |
|
| 1969-07-16 13:33:31 | | Maximum bending moment (33,200,000 lbf-in). |
|
| 1969-07-16 13:34:15 | | S-IC center engine cutoff command. Altitude 23.761nm. Downrange 25.067nm. Speed 5321ft/sec. |
|
| 1969-07-16 13:34:40 | | Pitch maneuver ended. |
|
| 1969-07-16 13:34:41 | | S-IC outboard engine cutoff. Altitude 35.701nm. Downrange 50.529nm. Speed 7852ft/sec. |
|
| 1969-07-16 13:34:41 | | S-IC maximum total inertial acceleration (3.94 g). |
|
| 1969-07-16 13:34:42 | | S-IC maximum Earth-fixed velocity. S-IC/S-II separation command. Altitude 36nm. Downrange 51nm. Speed 7883ft/sec. |
|
| 1969-07-16 13:34:43 | | S-II engine start command. |
|
| 1969-07-16 13:34:44 | | S-II ignition. |
|
| 1969-07-16 13:35:12 | | S-II aft interstage jettisoned. |
|
| 1969-07-16 13:35:17 | | Launch escape tower jettisoned. |
|
| 1969-07-16 13:35:24 | | Iterative guidance mode initiated. |
|
| 1969-07-16 13:36:29 | | S-IC apex. |
|
| 1969-07-16 13:39:40 | | S-II center engine cutoff. Altitude 97.28nm. Downrange 601.678nm. Speed 17405ft/sec. |
|
| 1969-07-16 13:39:40 | | S-II maximum total inertial acceleration (1.82 g). |
|
| 1969-07-16 13:41:03 | | S-IC impact (theoretical). |
|
| 1969-07-16 13:41:08 | | S-II outboard engine cutoff. Altitude 101.142nm. Downrange 873.886nm. Speed 21368ft/sec. |
|
| 1969-07-16 13:41:09 | | S-II maximum Earth-fixed velocity. S-II/S-IVB separation command. |
|
| 1969-07-16 13:41:09 | | S-IVB 1st burn start command. |
|
| 1969-07-16 13:41:12 | | S-IVB 1st burn ignition. |
|
| 1969-07-16 13:41:21 | | S-IVB ullage case jettisoned. |
|
| 1969-07-16 13:41:47 | | S-II apex. |
|
| 1969-07-16 13:43:39 | | S-IVB 1st burn cutoff. Altitude 103.202nm. Downrange 1421.96nm. Speed 24238ft/sec. |
|
| 1969-07-16 13:43:39 | | S-IVB 1st burn maximum total inertial acceleration (0.69 g). |
|
| 1969-07-16 13:43:49 | | Earth orbit insertion (100.4 x 98.9nm, 32.521 deg inclination). S-IVB 1st burn maximum Earth-fixed velocity. |
|
| 1969-07-16 13:43:59 | | Maneuver to local horizontal attitude started. |
|
| 1969-07-16 13:45:21 | | Orbital navigation started. |
|
| 1969-07-16 13:52:13 | | S-II impact (theoretical). |
|
| 1969-07-16 16:06:38 | | S-IVB 2nd burn restart preparation. |
|
| 1969-07-16 16:16:08 | | S-IVB 2nd burn restart command. |
|
| 1969-07-16 16:16:16 | | S-IVB 2nd burn ignition (STDV open). Speed 25560ft/sec |
|
| 1969-07-16 16:22:03 | | S-IVB 2nd burn cutoff. Speed 35568ft/sec. Inclination 31.386deg |
|
| 1969-07-16 16:22:03 | | S-IVB 2nd burn maximum total inertial acceleration (1.45 g). |
|
| 1969-07-16 16:22:03 | | S-IVB 2nd burn maximum Earth-fixed velocity. |
|
| 1969-07-16 16:22:03 | | S-IVB safing procedures started. |
|
| 1969-07-16 16:22:13 | | Translunar injection. Altitude 180.581nm. Speed 35546ft/sec. |
|
| 1969-07-16 16:22:23 | | Maneuver to local horizontal attitude started. |
|
| 1969-07-16 16:22:23 | | Orbital navigation started. |
|
| 1969-07-16 16:37:03 | | Maneuver to transposition and docking attitude started. |
|
| 1969-07-16 16:47:23 | | CSM separated from S-IVB. Altitude 3815nm. Speed 24963ft/sec. |
|
| 1969-07-16 16:49:04 | | CSM separation maneuver ignition. |
|
| 1969-07-16 16:49:11 | | CSM separation maneuver cutoff. |
|
| 1969-07-16 16:56:03 | | CSM docked with LM/S-IVB. Altitude 5318nm. Speed 22663ft/sec. |
|
| 1969-07-16 17:49:03 | | CSM/LM ejected from S-IVB. |
|
| 1969-07-16 18:12:01 | | CSM/LM evasive maneuver from S-IVB ignition. Altitude16621nm. Speed 14680ft/sec. |
|
| 1969-07-16 18:12:04 | | CSM/LM evasive maneuver from S-IVB cutoff. Altitude 16627nm. Speed 14663ft/sec. |
|
| 1969-07-16 18:13:07 | | S-IVB maneuver to lunar slingshot attitude initiated. |
|
| 1969-07-16 18:23:07 | | S-IVB lunar slingshot maneuver - LH2 tank CVS opened. |
|
| 1969-07-16 18:35:07 | | S-IVB lunar slingshot maneuver - LOX dump started. |
|
| 1969-07-16 18:36:55 | | S-IVB lunar slingshot maneuver - LOX dump ended. |
|
| 1969-07-16 19:09:47 | | S-IVB lunar slingshot maneuver - APS ignition. |
|
| 1969-07-16 19:14:27 | | S-IVB lunar slingshot maneuver - APS cutoff. |
|
| 1969-07-16 19:14:48 | | S-IVB maneuver to communications attitude initiated. |
|
| 1969-07-17 00:04:00 | | TV transmission started (recorded at Goldstone and transmitted to Houston at 011:26). |
|
| 1969-07-17 00:20:00 | | TV transmission ended. |
|
| 1969-07-17 16:16:58 | | Midcourse correction ignition. Altitude 109475nm. Speed 5025ft/sec. |
|
| 1969-07-17 16:17:01 | | Midcourse correction cutoff. Altitude 109447nm. Speed 5010ft/sec. |
|
| 1969-07-17 20:00:00 | | TV transmission started. |
|
| 1969-07-17 20:50:00 | | TV transmission ended. |
|
| 1969-07-17 23:31:00 | | TV transmission started. |
|
| 1969-07-18 00:07:00 | | TV transmission ended. |
|
| 1969-07-18 20:40:00 | | TV transmission started. |
|
| 1969-07-18 21:02:00 | | CDR and LMP entered LM for initial inspection. |
|
| 1969-07-18 22:16:00 | | TV transmission ended. |
|
| 1969-07-18 23:27:00 | | CDR and LMP entered CM. |
|
| 1969-07-19 03:11:55 | | Equigravisphere. |
|
| 1969-07-19 17:21:50 | | Lunar orbit insertion ignition. |
|
| 1969-07-19 17:27:47 | | Lunar orbit insertion cutoff. |
|
| 1969-07-19 18:45:00 | | Sighting of an illumination in the Aristarchus region. 1st time a lunar transient event sighted from space |
|
| 1969-07-19 19:52:00 | | TV transmission started. |
|
| 1969-07-19 20:14:00 | | S-IVB closest approach to lunar surface. |
|
| 1969-07-19 20:32:00 | | TV transmission ended. |
|
| 1969-07-19 21:43:36 | | Lunar orbit circularization ignition. |
|
| 1969-07-19 21:43:53 | | Lunar orbit circularization cutoff. |
|
| 1969-07-19 22:42:00 | | LMP entered CM for initial power-up and system checks. |
|
| 1969-07-20 01:07:00 | | LMP entered CM. |
|
| 1969-07-20 12:52:00 | | CDR and LMP entered LM for final preparations for descent. |
|
| 1969-07-20 14:32:00 | | LMP entered CM. |
|
| 1969-07-20 15:02:00 | | LMP entered LM. |
|
| 1969-07-20 15:17:00 | | LM system checks started. |
|
| 1969-07-20 17:32:00 | | LM system checks ended. |
|
| 1969-07-20 17:44:00 | | CSM/LM undocked. |
|
| 1969-07-20 18:11:52 | | CSM/LM separation maneuver ignition. |
|
| 1969-07-20 18:12:01 | | CSM/LM separation maneuver cutoff. |
|
| 1969-07-20 19:08:14 | | LM descent orbit insertion ignition (LM SPS). |
|
| 1969-07-20 19:08:44 | | LM descent orbit insertion cutoff. |
|
| 1969-07-20 19:49:17 | | LM acquisition of data. |
|
| 1969-07-20 19:52:53 | | LM landing radar on. |
|
| 1969-07-20 19:56:40 | | LM abort guidance aligned to primary guidance. |
|
| 1969-07-20 19:59:32 | | LM yaw maneuver to obtain improved communications. |
|
| 1969-07-20 20:04:55 | | LM altitude 50,000 feet. |
|
| 1969-07-20 20:04:58 | | LM propellant settling firing started. |
|
| 1969-07-20 20:05:05 | | LM powered descent engine ignition. |
|
| 1969-07-20 20:05:31 | | LM fixed throttle position. |
|
| 1969-07-20 20:09:59 | | LM face-up maneuver completed. |
|
| 1969-07-20 20:10:22 | | LM 1202 alarm. |
|
| 1969-07-20 20:10:45 | | LM radar updates enabled. |
|
| 1969-07-20 20:10:50 | | LM altitude less than 30,000 ft and velocity less than 2,000 ft/sec (landing radar velocity update started). |
|
| 1969-07-20 20:11:02 | | LM 1202 alarm. |
|
| 1969-07-20 20:11:31 | | LM throttle recovery. |
|
| 1969-07-20 20:13:32 | | LM approach phase entered. |
|
| 1969-07-20 20:13:37 | | LM landing radar antenna to position 2. |
|
| 1969-07-20 20:13:53 | | LM attitude hold mode selected (check of LM handling qualities). |
|
| 1969-07-20 20:14:03 | | LM automatic guidance enabled. |
|
| 1969-07-20 20:14:18 | | LM 1201 alarm. |
|
| 1969-07-20 20:14:19 | | LM landing radar switched to low scale. |
|
| 1969-07-20 20:14:43 | | LM 1202 alarm. |
|
| 1969-07-20 20:14:58 | | LM 1202 alarm. |
|
| 1969-07-20 20:15:09 | | LM landing point redesignation. |
|
| 1969-07-20 20:15:13 | | LM altitude hold. |
|
| 1969-07-20 20:15:20 | | LM abort guidance attitude updated. |
|
| 1969-07-20 20:15:22 | | LM rate of descent landing phase entered. |
|
| 1969-07-20 20:16:11 | | LM landing radar data not good. |
|
| 1969-07-20 20:16:21 | | LM landing data good. |
|
| 1969-07-20 20:16:28 | | LM fuel low-level quantity light. |
|
| 1969-07-20 20:16:35 | | 1st evidence of surface dust disturbed by descent engine. |
|
| 1969-07-20 20:16:59 | | LM landing radar data not good. |
|
| 1969-07-20 20:17:03 | | LM landing radar data good. |
|
| 1969-07-20 20:17:39 | | LM lunar landing. |
|
| 1969-07-20 20:17:41 | | LM powered descent engine cutoff. |
|
| 1969-07-20 22:12:00 | | Decision made to proceed with EVA prior to first rest period. |
|
| 1969-07-20 23:43:00 | | Preparation for EVA started. |
|
| 1969-07-21 02:39:33 | | EVA started (hatch open). |
|
| 1969-07-21 02:51:16 | | CDR completely outside LM on porch. |
|
| 1969-07-21 02:53:18 | | Modular equipment stowage assembly deployed (CDR). |
|
| 1969-07-21 02:54:00 | | First clear TV picture received. |
|
| 1969-07-21 02:55:28 | | CDR at foot of ladder (starts to report, then pauses to listen). |
|
| 1969-07-21 02:55:38 | | CDR at foot of ladder and described surface as “almost like a powder.” |
|
| 1969-07-21 02:56:15 | | 1st step taken lunar surface (CDR). “That’s one small step for a man…one giant leap for mankind.” |
|
| 1969-07-21 02:56:48 | | CDR started surface examination and description, assessed mobility and described effects of LM descent engine. |
|
| 1969-07-21 02:58:54 | | CDR ended surface examination. LMP started to send down camera. |
|
| 1969-07-21 03:02:23 | | Camera installed on RCU bracket, LEC stored on secondary strut of LM landing gear. |
|
| 1969-07-21 03:02:53 | | Surface photography (CDR). |
|
| 1969-07-21 03:05:58 | | Contingency sample collection started (CDR). |
|
| 1969-07-21 03:09:08 | | Contingency sample collection ended (CDR). |
|
| 1969-07-21 03:11:57 | | LMP started egress from LM. |
|
| 1969-07-21 03:13:56 | | LMP at top of ladder. Descent photographed by CDR. |
|
| 1969-07-21 03:15:16 | | LMP on lunar surface. |
|
| 1969-07-21 03:15:47 | | Surface examination and examination of landing effects on surface and on LM started (CDR, LMP). |
|
| 1969-07-21 03:21:06 | | Insulation removed from modular equipment stowage assembly (CDR). |
|
| 1969-07-21 03:23:35 | | TV camera focal distance adjusted (CDR). |
|
| 1969-07-21 03:24:19 | | Plaque unveiled (CDR). |
|
| 1969-07-21 03:24:40 | | Plaque read (CDR). |
|
| 1969-07-21 03:31:28 | | TV camera redeployed. Panoramic TV view started (CDR). |
|
| 1969-07-21 03:34:53 | | TV camera placed in final deployment position (CDR). |
|
| 1969-07-21 03:35:20 | | Solar wind composition experiment deployed (LMP). |
|
| 1969-07-21 03:41:43 | | United States flag deployed (CDR, LMP). |
|
| 1969-07-21 03:42:24 | | Evaluation of visibility in lunar sunlight (LMP). |
|
| 1969-07-21 03:45:15 | | Evaluation of surface mobility started (LMP). |
|
| 1969-07-21 03:48:02 | | Evaluation of surface mobility end (LMP). |
|
| 1969-07-21 03:48:30 | | Presidential message from White House and response from CDR. |
|
| 1969-07-21 03:50:21 | | Presidential message and CDR response ended. |
|
| 1969-07-21 03:52:06 | | Evaluation of trajectory of lunar soil when kicked (LMP) and bulk sample collection started (CDR). |
|
| 1969-07-21 03:57:09 | | Evaluation of thermal effects of sun and shadow inside the suit (LMP). |
|
| 1969-07-21 04:00:22 | | Evaluation of surface shadows and colors (LMP). |
|
| 1969-07-21 04:06:13 | | LM landing gear inspection and photography (LMP). |
|
| 1969-07-21 04:07:36 | | Bulk sample completed (CDR). |
|
| 1969-07-21 04:18:36 | | LM landing gear inspection and photography (CDR, LMP). |
|
| 1969-07-21 04:25:38 | | Scientific equipment bay doors opened. |
|
| 1969-07-21 04:27:42 | | Passive seismometer deployed. |
|
| 1969-07-21 04:35:57 | | Lunar ranging retroreflector deployed (CDR). |
|
| 1969-07-21 04:40:39 | | 1st passive seismic experiment data received on Earth. |
|
| 1969-07-21 04:43:00 | | Collection of documented samples started (CDR/LMP). |
|
| 1969-07-21 04:52:00 | | Solar wind composition experiment retrieved (LMP) . |
|
| 1969-07-21 05:01:39 | | LMP inside LM. |
|
| 1969-07-21 05:07:51 | | Transfer of sample containers reported complete. |
|
| 1969-07-21 05:09:32 | | CDR inside LM, assisted and monitored by LMP. |
|
| 1969-07-21 05:11:13 | | EVA ended (hatch closed). |
|
| 1969-07-21 07:37:00 | | LM equipment jettisoned. |
|
| 1969-07-21 17:54:00 | | LM lunar liftoff ignition (LM APS). |
|
| 1969-07-21 18:01:15 | | LM orbit insertion cutoff. |
|
| 1969-07-21 18:51:35 | | Coelliptic sequence initiation ignition. |
|
| 1969-07-21 18:52:22 | | Coelliptic sequence initiation cutoff. |
|
| 1969-07-21 19:49:49 | | Constant differential height maneuver ignition. |
|
| 1969-07-21 19:50:29 | | Constant differential height maneuver cutoff. |
|
| 1969-07-21 20:35:51 | | Terminal phase initiation ignition. |
|
| 1969-07-21 20:36:14 | | Terminal phase initiation cutoff. |
|
| 1969-07-21 20:50:30 | | LM 1st midcourse correction. |
|
| 1969-07-21 21:05:30 | | LM 2nd midcourse correction. |
|
| 1969-07-21 21:08:57 | | Braking started. |
|
| 1969-07-21 21:18:09 | | Terminal phase finalize ignition. |
|
| 1969-07-21 21:18:38 | | Terminal phase finalize cutoff. |
|
| 1969-07-21 21:24:05 | | Stationkeeping started. |
|
| 1969-07-21 21:35:00 | | CSM/LM docked. |
|
| 1969-07-21 22:52:00 | | CDR entered CM. |
|
| 1969-07-21 23:17:00 | | LMP entered CM. |
|
| 1969-07-21 23:41:31 | | LM ascent stage jettisoned. |
|
| 1969-07-22 00:02:01 | | CSM/LM final separation ignition. |
|
| 1969-07-22 00:02:08 | | CSM/LM final separation cutoff. |
|
| 1969-07-22 04:55:42 | | Transearth injection ignition (SPS). |
|
| 1969-07-22 04:58:13 | | Transearth injection cutoff. |
|
| 1969-07-22 20:01:57 | | Midcourse correction ignition. |
|
| 1969-07-22 20:02:07 | | Midcourse correction cutoff. |
|
| 1969-07-23 01:08:00 | | TV transmission started. |
|
| 1969-07-23 01:26:00 | | TV transmission ended. |
|
| 1969-07-23 22:42:00 | | TV transmission started. |
|
| 1969-07-23 22:45:00 | | TV transmission ended. |
|
| 1969-07-23 23:04:00 | | TV transmission started. |
|
| 1969-07-23 23:16:00 | | TV transmission ended. |
|
| 1969-07-24 16:21:12 | | CM/SM separation. |
|
| 1969-07-24 16:35:05 | | Entry. |
|
| 1969-07-24 16:39:00 | | Visual contact with CM established by aircraft. |
|
| 1969-07-24 16:40:00 | | Radar contact with CM established by recovery ship. |
|
| 1969-07-24 16:44:06 | | Drogue parachute deployed |
|
| 1969-07-24 16:46:00 | | VHF voice contact and recovery beacon contact established. |
|
| 1969-07-24 16:50:35 | | Splashdown (went to apex-down). |
|
| 1969-07-24 16:58:15 | | CM returned to apex-up position. |
|
| 1969-07-24 17:04 | | Flotation collar inflated. |
|
| 1969-07-24 17:21 | | Hatch opened for crew egress. |
|
| 1969-07-24 17:29 | | Crew egress. |
|
| 1969-07-24 17:53 | | Crew aboard recovery ship. |
|
| 1969-07-24 17:58 | | Crew entered mobile quarantine facility. |
|
| 1969-07-24 19:50 | | CM lifted from water. |
|
| 1969-07-24 19:58 | | CM secured to quarantine facility. |
|
| 1969-07-24 20:05 | | CM hatch reopened. |
|
| 1969-07-24 22:00 | | Sample return containers 1 and 2 removed from CM. |
|
| 1969-07-24 23:32 | | Container 1 removed from mobile quarantine facility. |
|
| 1969-07-25 00:05 | | Container 2 removed from mobile quarantine facility. |
|
| 1969-07-25 05:15 | | Container 2 and film flown to Johnston Island. |
|
| 1969-07-25 11:45 | | Container 1 flown to Hickam Air Force Base, Hawaii. |
|
| 1969-07-25 16:15 | | Container 2 and film arrived in Houston, TX. |
|
| 1969-07-25 23:13 | | Container 1, film, and biological samples arrived in Houston. |
|
| 1969-07-26 03:00 | | CM decontaminated and hatch secured. |
|
| 1969-07-26 04:35 | | Mobile quarantine facility secured. |
|
| 1969-07-27 00:15 | | Mobile quarantine facility and CM offloaded. |
|
| 1969-07-27 02:05 | | Safing of CM pyrotechnics completed. |
|
| 1969-07-28 06:00 | | Mobile quarantine facility arrived at Ellington AFB, Houston. |
|
| 1969-07-28 10:00 | | Crew in Lunar Receiving Laboratory, Houston |
|
| 1969-07-30 23:17 | | CM delivered to Lunar Receiving Laboratory. |
|
| 1969-08-03 11:58:46 | | Passive seismic experiment turned off. |
|
| 1969-08-10 | | Crew released from quarantine. |
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| 1969-08-14 | | CM delivered to contractor’s facility in Downey, CA. |
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| 1969-08-27 | | EASEP turned off by ground command. |