1994-062A
The STS-68 mission had an RSLS abort at T-1.9s on 1994 Aug 18 due to higher than expected temperatures on engine 2032. The launch was postponed until after the STS-64 flight. The second Space Radar Lab mission finally got off the ground at 1115.58 UT on 1994 Sep 30. SRB separation was at 0718 and MECO and ET separation came at 0724, leaving Endeavour in a 52 x 213 km x 57 deg orbit. The OMS 2 circularization burn was at MET 35:10, or 0751 UT. The orbit at Sep 30.70 was 213 x 226 km x 57.0 deg.
Trim burns were made on Oct 4 to adjust the orbit to match that of the STS-59 flight to within 10 meters. The orbit was lowered on Oct 7 for an interferometry experiment. A trim burn on Oct 9 adjusted the orbit again.
| STS-68 | |||
| Date | Time | Event | Orbit |
| 1994 Jul 21 | Tow to VAB | ||
| 1994 Aug 3 | Rollout | ||
| 1994 Aug 18 | 1053:58 | RSLS abort T-1.8s | LC39 |
| 1994 Aug 24 | Rollback | VAB | |
| 1994 Sep 30 | 1116:00 | Launch | LC39 |
| 1118:04 | SRB sep T+2:04 | ||
| 1124:35 | MECO T+8:35 | 87.24 49 x 226 x 57.0 (OMS dV) | |
| 1124:54 | ET sep | 52 x 213 x 57.0 | |
| 1126:35 | Prop dump | ||
| 1151:09 | OMS-2 1:39 49m/s | 88.90 214 x 226 x 57.01 | |
| 1249 | PLBD open | ||
| Activate radar | |||
| 1994 Oct 2 | 88.86 212 x 224 x 57.0 | ||
| 1994 Oct 5 | 88.80 209 x 221 x 57.0 | ||
| 1994 Oct 7 | 0600 | 88.76 206 x 219 x 57.0 | |
| Lower orbit | |||
| 1994 Oct 8 | 1600 | 88.61 199 x 212 x 57.0 | |
| 1994 Oct 10 | Deactivate radar payload | ||
| 1994 Oct 11 | 0600 | 88.60 198 x 211 x 57.0 | |
| 1206 | PLBD closed | ||
| 1607:19 | Deorbit 2:18 73m/s | -42 x 210 x 57 | |
| 1629:46 | Entry interface | ||
| 1702:09 | Landed | RW22 EAFB | |
| 1702:11 | Drag chute | ||
| 1702:21 | NGTD | ||
| 1703:10 | Wheels stop | ||
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