1987-075A
A month after the 9th FSW flight, a new Chinese recoverable satellite was launched. This was the first FSW-1 model. The recoverable capsule was about 1000 kg, 350 kg of retro solid fuel and 750 kg for the instrument module. The FSW-1 had improved avionics and attitude control as well as new payloads. Orbital altitude was lower; the mission lasted 8 days and was recovered on Sep 17.
| FSW-1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Sep 9 | 0715 | Launch by CZ2 | JQ |
| 0717 | T+2:10 MECO | ||
| 0717 | Stage 2 burn | ||
| 0719? | T+4:02? Stage 2 MECO | ||
| 0722? | Stage 2 VECO | ||
| 0722? | CZ-2C sep | 89.7 206 x 310 x 63.0 | |
| 1987 Sep 10 | 89.63 205 x 307 x 63.0 | ||
| 1987 Sep 16 | 0001 | 89.52 204 x 297 x 62.99 | |
| 1987 Sep 17 | 0422 | 89.49 202 x 295 x 62.99 | |
| 1987 Sep 17 | 0501 | Capsule landed in China | |
| 1987 Sep 18 | 75C,D cataloged | ||
| 89.41 202 x 288 x 62.99 | |||
| 1987 Sep 19 | 89.37 201 x 285 x 62.98 | ||
| 1987 Sep 22 | end of transmissions | ||
| 1987 Sep 30 | 88.56 183 x 223 x 62.97 | ||
| 1987 Oct 8 | Reentered | ||
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