Apollo 10 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 |
075:55:54.0 |
95.1 |
8,232.3 |
|
|
|
|
Lunar orbit insertion cutoff |
076:01:50.1 |
61.2 |
5,471.9 |
356.1 |
2,982.4 |
170.0 |
60.2 |
Lunar orbit circularization ignition |
080:25:08.1 |
60.4 |
5,484.7 |
|
|
|
|
Lunar orbit circularization cutoff |
080:25:22.0 |
59.3 |
5,348.9 |
13.9 |
139.0 |
61.0 |
59.2 |
CSM/LM undocked |
098:11:57 |
58.1 |
5,357.8 |
|
|
|
|
CSM/LM separation ignition |
098:47:17.4 |
59.2 |
5,352.2 |
|
|
|
|
CSM/LM separation cutoff |
098:47:25.7 |
59.2 |
5,352.1 |
8.3 |
2.5 |
62.9 |
57.7 |
LM descent orbit insertion ignition |
099:46:01.6 |
61.6 |
5,339.6 |
|
|
|
|
LM descent orbit insertion cutoff |
099:46:29.0 |
61.2 |
5,271.2 |
27.4 |
71.3 |
60.9 |
8.5 |
LM closest approach to lunar surface |
100:41:43 |
7.8 |
|
|
|
|
|
LM phasing ignition |
100:58:25.93 |
17.7 |
5,212.4 |
|
|
|
|
LM phasing cutoff |
100:59:05.88 |
19.0 |
5,672.9 |
39.95 |
176.0 |
190.1 |
12.1 |
LM ascent stage/descent stage separated |
102:45:16.9 |
31.4 |
5,605.6 |
|
|
|
|
LM ascent orbit insertion ignition |
102:55:02.13 |
11.6 |
5,705.2 |
|
|
|
|
LM ascent orbit insertion cutoff |
102:55:17.68 |
11.7 |
5,520.6 |
15.55 |
220.9 |
46.5 |
11.0 |
LM coelliptic sequence initiation ignition |
103:45:55.3 |
44.7 |
5,335.5 |
|
|
|
|
LM coelliptic sequence initiation cutoff |
103:46:22.6 |
44.6 |
5,381.7 |
27.3 |
45.3 |
48.7 |
40.7 |
LM constant differential height ignition |
104:43:53.28 |
44.3 |
5,394.7 |
|
|
|
|
LM constant differential height cutoff |
104:43:54.93 |
43.8 |
5,394.9 |
1.65 |
3.0 |
48.8 |
42.1 |
LM terminal phase initiation ignition |
105:22:55.58 |
48.4 |
5,369.2 |
|
|
|
|
LM terminal phase initiation cutoff |
105:23:12.08 |
47.0 |
5,396.7 |
16.50 |
24.1 |
58.3 |
46.8 |
LM 1st midcourse correction |
105:37:56 |
|
|
|
1.27 |
|
|
LM 2nd midcourse correction |
105:52:56 |
|
|
|
1.84 |
|
|
LM braking |
106:05:49 |
|
|
|
31.6 |
63.3 |
56.4 |
CSM/LM docked |
106:22:02 |
54.7 |
5,365.9 |
|
|
|
|
LM separation ignition |
108:43:23.3 |
57.3 |
5,352.3 |
|
|
|
|
LM separation cutoff |
108:43:29.8 |
57.6 |
5,352.1 |
6.5 |
2.1 |
64.0 |
56.3 |
LM ascent propulsion system ignition |
108:52:05.5 |
59.1 |
5,343.0 |
|
|
|
|
LM ascent propulsion system depletion |
108:56.14.5 |
89.7 |
9,056.4 |
249.0 |
4,600.0 |
-2,211.6 |
56.2 |