Apollo 16 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 |
000:00:00.59 |
0.060 |
0.000 |
0.0 |
1,340.7 |
|
28.4470 |
-80.6041 |
0.05 |
90.00 |
Mach 1 achieved |
000:01:07.5 |
4.282 |
1.358 |
1,076.4 |
2,075.5 |
|
28.4539 |
-80.5797 |
26.79 |
84.51 |
Maximum dynamic pressure |
000:01:26.0 |
7.755 |
3.800 |
1,759.6 |
2,785.9 |
|
28.4670 |
-80.5359 |
29.12 |
81.64 |
S-IC center engine cutoff* |
000:02:17.85 |
24.548 |
26.821 |
5,488.2 |
6,658.8 |
144.55 |
28.5847 |
-80.1207 |
23.105 |
76.125 |
S-IC outboard engine cutoff |
000:02:41.78 |
35.698 |
49.927 |
7,753.0 |
8,961.7 |
168.5 |
28.7009 |
-79.7028 |
19.914 |
75.328 |
S-IC/S-II separation* |
000:02:43.5 |
36.560 |
51.929 |
7,767.8 |
8,979.2 |
|
28.7109 |
-79.6666 |
19.643 |
75.339 |
S-II center engine cutoff |
000:07:41.77 |
92.441 |
592.660 |
17,039.0 |
18,357.7 |
296.57 |
30.9376 |
-69.6064 |
0.116 |
79.535 |
S-II outboard engine cutoff |
000:09:19.54 |
93.445 |
894.079 |
21,539.3 |
22,858.7 |
394.34 |
31.7737 |
-63.8100 |
0.367 |
82.585 |
S-II/S-IVB separation* |
000:09:20.5 |
93.468 |
897.389 |
21,550.4 |
22,869.8 |
|
31.7812 |
-63.7457 |
0.358 |
82.622 |
S-IVB 1st burn cutoff |
000:11:46.21 |
93.374 |
1,430.142 |
24,280.1 |
25,600.0 |
142.61 |
32.5109 |
-53.2983 |
0.001 |
88.496 |
Earth orbit insertion |
000:11:56.21 |
93.377 |
1,469.052 |
24,286.1 |
25,605.0 |
|
32.5262 |
-52.5300 |
0.001 |
88.932 |
*Only the commanded time is available for this event.