Apollo 15 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 |
000:00:00.58 |
0.060 |
0.000 |
1.5 |
1,340.7 |
|
28.4470 |
-80.6041 |
0.07 |
90.00 |
Mach 1 achieved |
000:01:05.0 |
4.224 |
1.004 |
1,052.0 |
2,028.1 |
|
28.4497 |
-80.5854 |
27.86 |
87.36 |
Maximum dynamic pressure |
000:01:22.0 |
7.401 |
2.970 |
1,661.1 |
2,681.3 |
|
28.4555 |
-80.5847 |
29.80 |
85.77 |
S-IC center engine cutoff* |
000:02:15.96 |
25.271 |
25.987 |
5,518.4 |
6,708.5 |
142.46 |
28.5203 |
-80.1190 |
24.217 |
82.494 |
S-IC outboard engine cutoff |
000:02:39.56 |
36.947 |
48.610 |
7,811.3 |
9,043.3 |
166.06 |
28.5824 |
-79.6961 |
21.266 |
82.129 |
S-IC/S-II separation* |
000:02:41.2 |
37.830 |
596.012 |
7,827.6 |
9,062.2 |
|
28.5876 |
-79.6605 |
21.021 |
82.144 |
S-II outboard engine cutoff |
000:09:09.06 |
95.184 |
874.532 |
21,588.4 |
22,949.6 |
386.06 |
29.6810 |
-63.9910 |
0.059 |
89.863 |
S-II/S-IVB separation* |
000:09:10.1 |
95.187 |
878.126 |
21,601.2 |
22,962.5 |
|
29.6811 |
-63.9221 |
0.047 |
89.900 |
S-IVB 1st burn cutoff |
000:11:34.67 |
93.215 |
1,406.808 |
24,236.4 |
25,596.7 |
141.47 |
29.2688 |
-53.8183 |
0.013 |
95.149 |
Earth orbit insertion |
000:11:44.67 |
93.215 |
1,445.652 |
24,242.4 |
25,602.6 |
|
29.2052 |
-53.0807 |
0.015 |
95.531 |
*Only the commanded time is available for this event.