2003-051A
A new generation FSW/JB satellite was launched by a CZ-2D with a stretched second stage in late 2003, shortly after the first piloted Shenzhou flight. It was reportedly designated Jianbing-4.
I speculate a slightly larger mass of 3200 kg for the JB-4, with a recoverable section mass of 1200 kg. Chen Lan reports the mass as 3800 kg and the launch vehicle as CZ-2D2 (an uprated second lot of CZ-2D rockets).
|
| FSW-3 |
| |
|
| Date | Time | Event | Orbit |
|---|
|
| 2003 Nov 3 | 0720 | Launch by CZ-2D |
| | 0730? | Stage 2 MECO |
| 2003 Nov 3 | | | 89.69 193 x 324 x 62.99 |
| 2003 Nov 4 | | | 89.78 193 x 333 x 62.99 |
| 2003 Nov 8 | 2154 | 89.75 192 x 331 x 62.99 |
| | | Apogee raise 4 km |
| 2003 Nov 9 | | | 89.79 192 x 335 x 62.99 |
| 2003 Nov 14 | | | 89.76 192 x 332 x 62.99 |
| | | Apogee raise 5 km |
| 2003 Nov 15 | | | 89.81 192 x 337 x 62.99 |
| 2003 Nov 20 | | | 89.70 191 x 328 x 62.99 |
| 2003 Nov 21 | 0142 | Deorbit command over 54N 80E |
| | | RV separation | -430? x 550? x 63.0 |
| 2003 Nov 21 | 0204 | Landed in Sichuan province |
| 2003 Nov 22 | | Apogee raise 29km |
| | | | 90.01 192 x 357 x 62.99 |
| 2003 Nov 28 | | | 89.82 190 x 340 x 62.98 |