Apollo 12 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 |
000:00:00.68 |
0.032 |
0.000 |
0.0 |
1,340.7 |
|
28.4470 |
-80.6041 |
0.07 |
90.00 |
1st lightning strike[1] |
000:00:36.5 |
1.053 |
0.062 |
387.9 |
1,445.7 |
|
28.4469 |
-80.6030 |
15.40 |
89.29 |
2nd lightning strike |
000:00:52 |
2.374 |
0.399 |
692.1 |
1,690.4 |
|
28.4487 |
-80.5968 |
22.74 |
87.32 |
Mach 1 achieved |
000:01:06.1 |
4.215 |
1.228 |
1,067.6 |
2,057.7 |
|
28.4532 |
-80.5820 |
27.13 |
84.84 |
Maximum dynamic pressure |
000:01:21.1 |
6.934 |
3.019 |
1,601.4 |
2,617.3 |
|
28.4627 |
-80.5498 |
29.02 |
82.10 |
S-IC center engine cutoff |
000:02:15.24 |
24.158 |
25.441 |
5,334.5 |
6,494.4 |
141.7 |
28.5794 |
-80.1463 |
23.944 |
76.115 |
S-IC outboard engine cutoff |
000:02:41.74 |
36.773 |
50.616 |
7,821.4 |
9,024.5 |
168.2 |
28.7069 |
-79.6913 |
20.513 |
75.231 |
S-IC/S-II separation |
000:02:42.4 |
37.118 |
51.338 |
7,850.3 |
9,054.2 |
|
28.7107 |
-79.6773 |
20.430 |
75.228 |
S-II center engine cutoff |
000:07:40.75 |
100.463 |
599.172 |
17,453.5 |
18,775.3 |
297.55 |
30.9599 |
-69.4827 |
0.502 |
79.632 |
S-II outboard engine cutoff |
000:09:12.34 |
102.801 |
884.711 |
21,508.8 |
22,831.7 |
389.14 |
31.7508 |
-63.9914 |
0.442 |
82.501 |
S-II/S-IVB separation |
000:09:13.20 |
102.827 |
887.667 |
21,517.8 |
22,840.7 |
|
31.7576 |
-63.9341 |
0.432 |
82.533 |
S-IVB 1st burn cutoff |
000:11:33.91 |
103.093 |
1,399.874 |
24,236.6 |
25,560.2 |
137.31 |
32.4933 |
-53.8956 |
-0.015 |
88.146 |
Earth orbit insertion |
000:11:43.91 |
103.086 |
1,438.608 |
24,242.3 |
25,565.9 |
|
32.5128 |
-53.1311 |
-0.014 |
88.580 |
[1]Data for this event reflects post flight trajectory reconstruction for 36 seconds Ground Elapsed Time.