Apollo 12 Lunar Orbit Phase
|
Event |
GET (hhh:mm:ss) |
Altitude (n mi) |
Space Fixed Velocity (ft/sec) |
Event Duration (sec) |
Velocity Change (ft/sec) |
Apolune (n mi) |
Perilune (n mi) |
|
Lunar orbit insertion ignition |
083:25:23.36 |
83.91 |
8,173.6 |
|
|
NA |
64.94 |
|
Lunar orbit insertion cutoff |
083:31:15.61 |
62.91 |
5,470.1 |
352.25 |
2,889.5 |
170.20 |
61.66 |
|
Lunar orbit circularization ignition |
087:48:48.08 |
62.79 |
5,470.6 |
|
|
170.37 |
61.42 |
|
Lunar orbit circularization cutoff |
087:49:04.99 |
62.74 |
5,331.4 |
16.91 |
165.2 |
66.10 |
54.59 |
|
CSM/LM undocked |
107:54:02.3 |
63.02 |
5,329.0 |
|
|
63.08 |
56.91 |
|
CSM/LM separation ignition |
108:24:36.8 |
59.22 |
5,350.0 |
|
|
63.91 |
56.99 |
|
CSM/LM separation cutoff |
108:24:51.2 |
59.15 |
5,350.5 |
14.4 |
2.4 |
64.06 |
56.58 |
|
LM descent orbit insertion ignition |
109:23:39.9 |
60.52 |
5,343.0 |
|
|
63.27 |
57.25 |
|
LM descent orbit insertion cutoff |
109:24:08.9 |
61.52 |
5,268.0 |
29.0 |
72.4 |
61.53 |
8.70 |
|
LM powered descent initiation |
110:20:38.1 |
7.96 |
5,566.4 |
|
|
62.30 |
7.96 |
|
LM powered descent cutoff |
110:32:35.1 |
|
|
717.0 |
|
|
|
|
CSM plane change ignition |
119:47:13.23 |
62.20 |
5,333.5 |
|
|
62.50 |
57.61 |
|
CSM plane change cutoff |
119:47:31.46 |
62.20 |
5,683.4 |
18.23 |
349.9 |
62.50 |
57.60 |
|
LM lunar liftoff ignition |
142:03:47.78 |
|
|
|
|
|
|
|
LM orbit insertion |
142:10:59.9 |
9.97 |
5,542.5 |
|
6,057 |
51.93 |
9.21 |
|
LM ascent stage cutoff |
142:11:01.78 |
|
|
434 |
|
|
|
|
LM coelliptic sequence initiation ignition |
143:01:51.0 |
51.46 |
5,310.3 |
|
|
52.51 |
9.94 |
|
LM coelliptic sequence initiation cutoff |
143:02:32.1 |
51.48 |
5,354.9 |
41.1 |
45 |
51.49 |
41.76 |
|
LM constant differential height ignition |
144:00:02.6 |
|
|
|
|
|
|
|
LM constant differential height cutoff |
144:00:15.6 |
|
|
13.0 |
13.8 |
44.40 |
40.40 |
|
LM terminal phase initiation ignition |
144:36:26 |
44.50 |
5,382.5 |
|
|
44.73 |
40.91 |
|
LM terminal phase initiation cutoff |
144:36:52 |
|
|
26.0 |
29 |
60.20 |
43.80 |
|
LM 1st midcourse correction |
144:51:29 |
|
|
|
|
|
|
|
LM 2nd midcourse correction |
145:06:29 |
|
|
|
|
|
|
|
LM terminal phase finalize ignition |
145:19:29.3 |
|
|
|
|
|
|
|
LM terminal phase finalize cutoff |
145:20:07.3 |
|
|
38.0 |
40 |
62.30 |
58.30 |
|
CSM/LM docked |
145:36:20.2 |
58.14 |
5,357.1 |
|
|
63.43 |
58.04 |
|
LM ascent stage jettison |
147:59:31.6 |
|
|
|
|
|
|
|
CSM/LM separation ignition |
148:04:30.9 |
59.94 |
5,347.4 |
|
|
64.66 |
59.08 |
|
CSM/LM separation cutoff |
148:04:36.3 |
|
|
5.4 |
1.0 |
62.00 |
57.50 |
|
LM ascent stage deorbit ignition |
149:28:14.8 |
57.62 |
5,361.8 |
|
|
63.52 |
57.94 |
|
LM ascent stage deorbit cutoff |
149:29:36.9 |
57.42 |
5,176.8 |
82.1 |
196.2 |
57.59 |
-63.15 |
|
CSM orbit plane change ignition |
159:04:45.47 |
58.70 |
5,353.2 |
|
|
64.23 |
56.58 |
|
CSM orbit plane change cutoff |
159:05:04.72 |
58.90 |
5,353.0 |
19.25 |
381.8 |
64.66 |
56.81 |