Summary of Maneuvers
| T + Time | Event | Burn Time | Delta-Velocity | Orbit |
|---|---|---|---|---|
| T + 00:00:00 | Lift-off | |||
| T + 00:02:14.34 | S-IC center engine cut-off | 141 s | ||
| T + 00:02:42.76 | S-IC engine cut-off | 169 s | ||
| T + 00:02:45.16 | S-II ignition | |||
| T + 00:03:13.5 | S-II skirt separation | |||
| T + 00:03:18.3 | LES jettison | |||
| T + 00:08:56.22 | S-II cut-off | |||
| T + 00:08:57 | S-II cutoff + separation, S-IVB ignition | |||
| T + 00:11:04.66 | S-IVB cutoff + orbital insertion | 127.4 s | 191.3 × 189.5 km | |
| T + 02:41:16 | CSM/S-IVB separation | |||
| T + 03:01:59.3 | CSM/LM docking | |||
| T + 04:08:09 | Spacecraft/S-IVB separation | |||
| T + 05:59:01.07 | First Service Propulsion System (SPS) test | 5.1 s | +10.4 m/s | 234.1 × 200.7 km |
| T + 22:13:04.07 | Second SPS test | 110 s | +259.2 m/s | 351.5 × 199.5 km |
| T + 25:17:39.27 | Third SPS test | 281.6 s | +782.6 m/s | 503.4 × 202.6 km |
| T + 28:24:41.37 | Fourth SPS test | 28.2 s | -914.5 m/s | 502.8 × 202.4 km |
| T + 49:41:34.46 | Docked DPS test | 369.7 s | -530.1 m/s | 499.3 × 202.2 km |
| T + 54:26:12.27 | Fifth SPS test | 43.3 s | -175.6 m/s | 239.3 × 229.3 km |
| T + 92:39:36 | CSM/LM undocking | |||
| T + 93:02:54 | CSM separation maneuver | 10.9 s | -1.5 m/s | |
| T + 93:47:35.4 | LM Descent Propulsion System (DPS) phasing maneuver | 18.6 s | +27.6 m/s | 253.5 × 207 km |
| T + 95:39:08.6 | LM DPS insertion maneuver | 22.2 s | +13.1 m/s | 257.2 × 248.2 km |
| T + 96:16:06.54 | LM concentric sequence initiation maneuver/Descent stage jettison | 30.3 s | -12.2 m/s | 255.2 × 208.9 km |
| T + 96:58:15 | LM Ascent Propulsion System (APS) constant delta height maneuver | 2.9 s | -12.6 m/s | 215.6 × 207.2 km |
| T + 97:57:59 | LM terminal phase finalization maneuver | 34.7 s | +6.8 m/s | 232.8 × 208.5 km |
| T + 99:02:26 | CSM/LM docking | |||
| T + 101:22:45 | LM ascent stage jettison | |||
| T + 101:32:44 | Post-jettison CSM separation maneuver | 7.2 s | +0.9 m/s | 235.7 × 224.6 km |
| T + 101:53:15.4 | LM APS burn to depletion | 350 s | +1,643.2 m/s | 6,934.4 × 230.6 km |
| T + 123:25:06.97 | Sixth SPS test | 1.29 s | -11.5 m/s | 222.6 × 195.2 km |
| T + 169:39:00.36 | Seventh SPS test | 25 s | +199.6 m/s | 463.4 × 181.1 km |
| T + 240:31:14.84 | Deorbit burn (SPS) | 11.6 s | -99.1 m/s | 442.2 × -7.8 km |
| T + 240:36:03.8 | SM jettison | |||
| T + 241:00:54 | Splashdown |
Read more about this topic: Apollo 9
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