Apollo 9

**Apollo 9**
Mission insignia
Missing image Apollo-9-patch.jpg Apollo 9 insignia
Mission statistics
Mission name:	Apollo 9
Call sign:	Command module: Gumdrop Lunar module: Spider
Number of crew:	3
Launch:	March 3, 1969 16:00:00 UTC Kennedy Space Center LC 39A
EVA length:	1 h 8 min 1 s
Splashdown:	March 13, 1969 17:00:54 UTC 23° 15' N - 67° 56' W
Duration:	10 d 1 h 0 min 54 s
Number of orbits:	152
Mass:	CSM 26,801 kg; LM 14,575 kg
Crew picture
Missing image GPN-2000-001162.jpg Apollo 9 crew portrait (L-R: McDivitt, Scott and Schweickart) Apollo 9 crew portrait (L-R: McDivitt, Scott and Schweickart)
Apollo 9 Crew

Apollo 9 was the third manned mission in the Apollo program, a ten day earth-orbital mission launched 3 March 1969. It was the second manned flight of the Saturn V launch vehicle and the first manned flight of the Apollo Lunar Module (LM).

Contents

1 Crew

1.1 Backup crew
1.2 Support crew

2 Mission parameters

2.1 LM - CSM docking
2.2 EVA
2.3 See also

3 Mission highlights

4 Original mission profile

5 Apollo 9 maneuver summary

5.1 Reference

6 External link

Crew

James McDivitt (flew on Gemini 4 & Apollo 9), commander
David Scott (flew on Gemini 8, Apollo 9, & Apollo 15), command module pilot
Russell Schweickart (flew on Apollo 9), lunar module pilot

Backup crew

Pete Conrad, commander
Dick Gordon, command module pilot
Alan Bean, lunar module pilot

Support crew

Mission parameters

Mass: CSM 26,801 kg; LM 14,575 kg
Perigee: 189.5 km
Apogee: 192.4 km
Inclination: 32.57°
Period: 88.64 min

LM - CSM docking

Undocked: March 7, 1969 - 12:39:36 UTC
Re-docked:March 7, 1969 - 19:02:26 UTC

EVA

Schweickart - EVA - LM forward hatch
- Start: March 6, 1969, 16:45:00 UTC
- End: March 6, 1969, 17:52:00 UTC
- Duration: 1 hour, 07 minutes
Scott - EVA - CM side hatch
- Start: March 6, 1969, 17:01:00 UTC
- End: March 6, 1969, 18:02:00 UTC
- Duration: 1 hour, 01 minute

Mission highlights

Apollo 9 was the first space test of the third critical piece of Apollo hardware-the lunar module. For ten days, the astronauts put all three Apollo vehicles through their paces in Earth orbit, undocking and then redocking the lunar lander with the command module, just as they would in lunar orbit. For this and all subsequent Apollo flights, the crews were allowed to name their own spacecraft. The gangly lunar module was "Spider," the command module "Gumdrop" on account of the blue cellophane wrapping in which the craft arrived at KSC. Schweickart and Scott performed a space walk, and Schweickart checked out the new Apollo spacesuit, the first to have its own life support system rather than being dependent on an umbilical connection to the spacecraft. Apollo 9 gave proof that the Apollo machines were up to the task of orbital rendezvous and docking.

Crew members tested the LM and practiced separation and docking maneuvers in earth orbit. The splashdown point was 23 deg 15 min N, 67 deg 56 min W, 180 miles (290 km) east of Bahamas and within sight of the recovery ship USS Guadalcanal.

The command module was displayed at the Michigan Space and Science Center, Jackson, Michigan until April 2004 when the center closed. In May, 2004, the command module Gumdrop was moved to San Diego Aerospace Museum in southern California. The LM ascent stage orbit decayed on 23 October 1981, the LM descent stage (1969-018D) orbit decayed 22 March 1969. The S-IVB stage J-2 engine was restarted after Lunar Module extraction and propelled the stage into solar orbit by burning to depletion.

Launched: March 3, 1969 from Pad 39A

Returned: March 13, 1969

Crew members: James McDivitt, commander; David Scott, command module pilot; Rusty Schweickart, lunar module pilot.

Command module: Gumdrop

Lunar module: Spider

Original mission profile

In October 1967 it was planned that following the first manned orbital flight of the CSM (Apollo 7) the second manned Apollo mission would have a manned CSM launched on a Saturn 1B and a few days later the Lunar Module Launched on a second Saturn 1B to practise first orbit rendevous. When the mission was delayed due to production problems with the LM McDivitt was offered the chance to fly the first manned Saturn V as Commander of Apollo 8 but declined. This had long lasting consequence as the crew rotation for Apollos 8 and 9 were swapped putting Neil Armstrong in line for the first manned landing mission.

Schweickart was due to carry out a more extensive set of space walk activity to test the Apollo suit but as he was suffering from space sickness this was restricted to the stand up test in the Lunar Module hatch.

Apollo 9 maneuver summary

T + Time	Event	Burn Time	Delta-Velocity	Orbit
T + 00:00:00	Lift-off	.	.	.
T + 00:02:14	S-IC center engine cut-off	141 s	.	.
T + 00:02:43	S-IC engine cut-off	169 s	.	.
T + 00:02:44	S-II ignition	.	.	.
T + 00:03:14	S-II skirt separation	.	.	.
T + 00:03:19	LES jettison	.	.	.
T + 00:08:56	S-II cut-off	.	.	.
T + 00:08:57	S-II cutoff + separation, S-IVB ignition	.	.	.
T + 00:11:05	S-IVB cutoff + orbital insertion	127.4 s	.	191.3 x 189.5 km
T + 02:45:00	CSM/S-IVB separation	.	.	.
T + 03:02:08	CSM/LM docking	.	.	.
T + 04:18:00	Spacecraft/S-IVB separation	.	.	.
T + 05:59:00	First SPS test	5.1 s	+10.4 m/s	234.1 x 200.7 km
T + 22:12:03	Second SPS test	110 s	+259.2 m/s	351.5 x 199.5 km
T + 25:17:38	Third SPS test	281.6 s	+782.6 m/s	503.4 x 202.6 km
T + 28:24:40	Fourth SPS test	28.2 s	-914.5 m/s	502.8 x 202.4 km
T + 49:41:33	First DPS test	369.7 s	-530.1 m/s	499.3 x 202.2 km
T + 54:26:11	Fifth SPS test	43.3 s	-175.6 m/s	239.3 x 229.3 km
T + 92:39:30	CSM/LM undocking	.	.	.
T + 93:02:53	CSM separation maneuver	10.9 s	-1.5 m/s	.
T + 93:47:34	LM DPS phasing maneuver	18.6 s	+27.6 m/s	253.5 x 207 km
T + 95:39:07	LM DPS insertion maneuver	22.2 s	+13.1 m/s	257.2 x 248.2 km
T + 96:16:04	LM concentric sequence initiation maneuver	30.3 s	-12.2 m/s	255.2 x 208.9 km
T + 96:58:14	LM APS constant delta height maneuver	2.9 s	-12.6 m/s	215.6 x 207.2 km
T + 97:57:59	LM terminal phase finalization maneuver	34.7 s	+6.8 m/s	232.8 x 208.5 km
T + 98:59:00	CSM/LM docking	.	.	.
T + 101:32:44	Post-jettison CSM separation maneuver	7.2 s	+0.9 m/s	235.7 x 224.6 km
T + 101:53:20	LM APS burn to depletion	350 s	+1,643.2 m/s	6,934.4 x 230.6 km
T + 123:25:06	Sixth SPS test	1.29 s	-11.5 m/s	222.6 x 195.2 km
T + 169:38:59	Seventh SPS test	25 s	+199.6 m/s	463.4 x 181.1 km
T + 240:31:14	Eighth SPS test	11.6 s	-99.1 m/s	442.2 x -7.8 km
T + 241:00:54	Splashdown	.	.	.