Apollo 10 Translunar Phase
Event |
GET (hhh:mm:ss) |
Altitude (n mi) |
Space Fixed Velocity (ft/sec) |
Event Duration (sec) |
Velocity Change (ft/sec) |
Space Fixed Flight Path Angle (deg) |
Space Fixed Heading Angle (E of N) |
Translunar injection |
002:39:20.58 |
179.920 |
35,562.96 |
|
|
7.379 |
61.065 |
CSM separated from S-IVB (ignition) |
003:02:42.4 |
3,502.626 |
25,548.72 |
|
|
43.928 |
67.467 |
CSM SPS evasive maneuver ignition |
004:39:09.8 |
17,938.5 |
14,220.2 |
|
|
65.150 |
91.21 |
CSM SPS evasive maneuver cutoff |
004:39:12.7 |
17,944.7 |
14,203.7 |
2.9 |
18.8 |
65.100 |
91.22 |
Midcourse correction ignition |
026:32:56.8 |
110,150.2 |
5,094.4 |
|
|
77.300 |
108.36 |
Midcourse correction cutoff |
026:33:03.9 |
110,155.9 |
5,110.0 |
7.1 |
49.2 |
77.800 |
108.92 |