1965-060A
Saturn SA-10 was launched at 1300:01 on 1965 Jul 30 and reached orbit at 1310:34. The orbital parameters were 95.52 min, 535 x 667 km x 28.8 deg. The Apollo BP-9A CSM separated from the Saturn S-4-10 stage and the cylindrical SMA (Service Module Adapter), allowing the Pegasus III MMC (micrometeoroid mounting capsule) payload to deploy. Pegasus III remained attached to the Saturn. It reentered on 1969 Aug 4. The mission was known as Apollo-Saturn 104 (AS-104).
| SA-10 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 Jul 30 | 1300:01 | Launch by Saturn I | KSC |
| 1302:23 | T+2:22 IECO | ||
| 1302:29 | T+2:28 OECO | ||
| 1302:30 | T+2:29 S-I sep | -6070 x 262 | |
| 1302:31 | S-IV burn | ||
| 1302:42 | Ullage motors sep | ||
| 1302:42 | LES sep | ||
| 1305:54 | S-I apogee 262 km | ||
| 1310:30 | S-IV-10 ECO | ||
| 1310:41 | Orbit insertion | ||
| 1312:05 | S-I impact | ||
| 1313:32 | LH2 NPV venting complete | ||
| 1313:33 | Pegasus C forward restraint sep | ||
| 1313:33 | Apollo BP-9A sep | ||
| 1314:33 | Pegasus C wing deploy | ||
| 1315:12 | Pegasus C wing complete | ||
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