Apollo 12 Transearth 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) |
Transearth injection ignition |
172:27:16.81 |
63.6 |
5,322.9 |
|
|
-0.202 |
-115.73 |
Transearth injection cutoff |
172:29:27.13 |
66.0 |
8,350.4 |
130.32 |
3,042.0 |
2.718 |
-116.45 |
Midcourse correction ignition |
188:27:15.8 |
180,031.2 |
3,035.6 |
|
|
-78.444 |
91.35 |
Midcourse correction cutoff |
188:27:20.2 |
180,029.0 |
3,036.0 |
4.4 |
2.0 |
-78.404 |
91.36 |
Midcourse correction ignition |
241:21:59.7 |
25,059.0 |
12,082.9 |
|
|
-68.547 |
96.00 |
Midcourse correction cutoff |
241:22:05.4 |
25,048.3 |
12,084.7 |
5.7 |
2.4 |
-68.547 |
96.01 |
CM/SM separation |
244:07:20.1 |
1,949.5 |
29,029.1 |
|
|
-36.454 |
98.17 |