1992-051A
The first FSW-2 engineering test flight was orbited in Aug 1992. Mass was 2590 kg. The FSW-2 used the standard FSW recovery capsule attached to a retrograde module and an equipment module. The equipment module carried a monopropellant orbit adjust system.
| FSW 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1992 Aug 9 | 0800 | Launch by CZ2D | JQ |
| 0802 | T+2:10 MECO | ||
| 0802 | Stage 2 burn | ||
| 0805? | MECO | ||
| 0809? | Stage 2 VECO | ||
| 0809? | Stage 2 sep | 175 x 330 x 63 | |
| 1992 Aug 12 | 89.44 170 x 323 x 63.1 | ||
| Orbit raise | 89.70 171 x 347 x 63.1 | ||
| 1992 Aug 15 | 89.64 170 x 343 x 63.1 | ||
| 1992 Aug | Maneuver engine failed | ||
| 1992 Aug 20 | 169 x 335 x 63.1 | ||
| 1992 Aug 24 | 0841 | 89.35 167 x 316 x 63.1 | |
| 1992 Aug 25 | 0310? | EM sep | |
| 0305? | Deorbit | ||
| 0305? | Retrograde module sep | ||
| 0308? | Reentry | ||
| 0320 | Capsule recovered | ||
| 1992 Aug 25 | 2153 | 89.23 170 x 302 x 63.0 | |
| 1992 Sep 1 | 87.27 129 x 149 x 63.0 | ||
| 1992 Sep 1 | Reentered | ||
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