Apollo 7 Ascent Phase
Event |
GET (hhh:mm:ss) |
Altitude (n mi) |
Range (n mi) |
Earth Fixed Velocity (ft/sec) |
Space Fixed Velocity (ft/sec) |
Event Duration (sec) |
Geocentric Latitude (deg N) |
Longitude (deg E) |
Space Fixed Flight Path Angle (deg) |
Space Fixed Heading Angle (E of N) |
Liftoff[1] |
000:00:00.36 |
0.019 |
0.000 |
0.0 |
1,341.7 |
|
28.3608 |
-80.5611 |
0.06 |
90.01 |
Mach 1 achieved |
000:01:02.15 |
4.120 |
0.753 |
1,039.1 |
1,960.1 |
|
28.3649 |
-80.5477 |
29.63 |
86.70 |
Maximum dynamic pressure |
000:01:15.5 |
6.567 |
1.933 |
1,459.4 |
2,408.8 |
|
28.3708 |
-80.5264 |
31.64 |
83.65 |
S-IB center engine cutoff |
000:02:20.65 |
30.626 |
29.184 |
6,264.7 |
7,394.5 |
123.64 |
28.5090 |
-80.0349 |
27.09 |
75.87 |
S-IB outboard engine cutoff |
000:02:24.32 |
32.678 |
32.418 |
6,479.1 |
7,616.8 |
147.31 |
28.5252 |
-79.9765 |
26.55 |
75.78 |
S-IB/S-IVB separation[2] |
000:02:25.59 |
33.389 |
33.561 |
6,472.1 |
7,612.6 |
|
28.5310 |
-79.9558 |
26.32 |
75.79 |
S-IVB engine cutoff |
000:10:16.76 |
123.167 |
983.290 |
24,181.2 |
25,525.9 |
469.79 |
31.3633 |
-61.9777 |
0.00 |
85.91 |
Earth orbit insertion |
000:10:26.76 |
123.177 |
1,121.743 |
24,208.5 |
25,553.2 |
|
31.4091 |
-61.2293 |
0.005 |
86.32 |