1965-068A
Gemini V was a long duration buildup mission. Cooper and Conrad's unofficial patch read `Eight days or bust'. Shortly after orbit insertion, a fuel cell heater failed; the spacecraft was put in a low power mode but the mission was allowed to continue. At 1613 the Radar (or Rendezvous) Evaluation Pod was ejected, but because of the power problems the radar could not be tested. A little over 1 day into the mission, Houston decided to abandon any plan to rendezvous with REP. Tests were made during a pass over Florida with a spare REP at KSC, confirming that the Gemini radar could pick up its L-band signal. On Aug 23, the craft made 5 burns over 2 hr to rendezvous with a simulated Agena target. On Aug 24 and 25, the astronauts tested their visual acuity, observing the Earth's surface. This included spotting a Minuteman missile launch. Further radar tests continued throughout the mission as the astronauts beat the Vostok-5 duration record.
For the first time the OAMS perigee lowering maneuver prior to retrofire was omitted. Retrofire was 82m/s aft and 55m/s down. Gemini V splashed down at 29 44 N 69 45 W in the Atlantic near the USS Lake Champlain, after a flight lasting 190 h 55 m 14 s.
| GT-5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 Aug 21 | 1359:59 | Launch | |
| 1402:33 | T+2:34 BECO | -5936 x 128 x 32.4 | |
| 1402:33 | Stage 1 sep | ||
| 1403:26 | T+3:27 Horizon sensor and radar cover fairings jettisoned | ||
| 1405:32 | T+5:33 SECO, Orbit insertion | 162 x 349 x 32.6 (NASA) | |
| 1405:55 | T+5:56 Stage 2 sep | ||
| 1405:55 | IVAR | 157 x 368 x 32.6 | |
| 1406:06 | OAMS off | ||
| 1426 | Fuel cell heater failed | ||
| 1456:00 | Perigee adjust burn 3m/s at apogee | 171 x 350 x 32.6 (NASA) | |
| 1517 | 89.58 169 x 338 x 32.6 | ||
| 1539? | Geometric experiment door jettison | ||
| 1607:15 | REP cover ejected | ||
| 1607:15 | REP deployed. 1.2m/s | ||
| 1621 | REP at 1km | ||
| 1965 Aug 22 | 0442 | 89.54 166 x 336 x 32.6 | |
| 1965 Aug 23 | 0433 | 89.52 170 x 330 x 32.6 | |
| Rendezvous burns | |||
| 1649:57 | HAdj 6.4m/s 28s lower apogee | 166 x 311 x 32.6 | |
| 1734:31 | Apogee burn 4.5m/s 20s | 183 x 311 x 32.6 | |
| 1806:26 | Plane change 5m/s 19s, 0.02deg change | ||
| 1904:04 | NSR Reverse Coelliptic 6.0m/s 22s | 198 x 311 x 32.6 | |
| Rendezvous with phantom target | |||
| 2000 | Observe Minuteman launch from CC | ||
| 1965 Aug 24 | 1318 | 89.55 197 x 306 x 32.61 | |
| 1633:04 | Stage 2 reentry | ||
| 1636 | Stage 2 breaks up over IOR 24S 108E | ||
| 1637 | Observe MM launch from VAFB | ||
| 1965 Aug 25 | 1628 | Observe MM launch from VAFB | |
| 1965 Aug 26 | 0829 | 89.46 199 x 295 x 32.6 | |
| 1965 Aug 29 | 1226:51 | Adapter module sep | |
| 1227:43 | Retrofire | ||
| 1228:00 | Retrofire complete | -70 x 295 x 32.6 | |
| 1228:32 | Retro module sep | ||
| 1242? | 120 km entry interface | ||
| 1255:14 | Splashdown in Atlantic | ||
| 1330 | Recovered by USS Lake Champlain | ||
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