1982-090A
FSW No. 5 (PRC 10) was launched in Sep 1982 on a 5 day mission. The new spacecraft had a CCD camera as well as the standard film camera. The apogee was reduced by 80 km relative to earlier flights.
A debris object was cataloged as decaying on Sep 11, 2 days after launch, from an 860 km apogee orbit. It may have been a separation motor cover.
| FSW | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1982 Sep 9 | 0719 | Launch by CZ2 | JQ |
| 0721 | T+2:10 MECO | ||
| 0721 | Stage 2 burn | ||
| 0723? | T+4:02? Stage 2 MECO | ||
| 0726? | Stage 2 VECO | ||
| 0726? | CZ-2C sep | 90.20 180 x 390 x 63.0 | |
| 1982 Sep 11 | 90C | 123 x 860 x 62.2 | |
| 1982 Sep 13 | 89.98 173 x 373 x 62.98 | ||
| 1982 Sep 14 | 0554? | Capsule sep | 89.74 170 x 355 x 63.0 |
| 0554? | RV retro | ||
| 0556? | Reentry | ||
| 0604 | Capsule landed in China | ||
| 1982 Sep 16 | 89.43 166 x 326 x 63.0 | ||
| 1982 Sep 21 | Reentered | 87.3 127 x 156 x 63.0 | |
No comments:
Post a Comment