Apollo 10 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 |
0.035 |
0.000 |
1.3 |
1,340.4 |
|
28.4658 |
-80.6209 |
0.06 |
90.00 |
Mach 1 achieved |
000:01:06.8 |
4.244 |
1.037 |
1,057.9 |
2,028.6 |
|
28.4714 |
-80.6023 |
27.82 |
85.03 |
Maximum dynamic pressure |
000:01:22.6 |
7.137 |
2.893 |
1,623.4 |
2,645.8 |
|
28.4813 |
-80.5690 |
28.83 |
82.23 |
S-IC center engine cutoff* |
000:02:15.16 |
23.430 |
25.009 |
5,299.0 |
6,473.20 |
141.56 |
28.5967 |
-80.1577 |
22.807 |
76.461 |
S-IC outboard engine cutoff |
000:02:41.63 |
35.247 |
50.419 |
7,810.2 |
9,028.58 |
168.03 |
28.7182 |
-79.7090 |
18.946 |
75.538 |
S-IC/S-II separation* |
000:02:42.31 |
35.580 |
51.223 |
7,833.4 |
9,052.79 |
|
28.7222 |
-79.6943 |
18.848 |
75.538 |
S-II center engine cutoff |
000:07:40.61 |
96.710 |
599.079 |
17,310.1 |
18,630.15 |
296.56 |
30.9579 |
-69.4941 |
1.029 |
79.585 |
S-II outboard engine cutoff |
000:09:12.64 |
101.204 |
883.670 |
21,309.9 |
22,632.02 |
388.59 |
31.7505 |
-64.0222 |
0.741 |
82.458 |
S-II/S-IVB separation |
000:09:13.50 |
101.247 |
886.634 |
21,317.8 |
22,639.93 |
|
31.7574 |
-63.9647 |
0.730 |
82.490 |
S-IVB 1st burn cutoff* |
000:11:43.76 |
103.385 |
1,430.977 |
24,238.8 |
25,562.40 |
146.95 |
32.5150 |
-53.2920 |
-0.0064 |
88.497 |
Earth orbit insertion |
000:11:53.76 |
103.334 |
1,469.790 |
24,244.3 |
25,567.88 |
|
32.5303 |
-52.5260 |
-0.0049 |
89.933 |
*Only the commanded time is available for this event.