ZX 6A (ChinaSat 6A)
ZX 6A [CAST]
ZX 6A (ChinaSat 6A) (formerly Sinosat-6, Xinnuo 6) is based upon a DFH-4 bus and will embark a hybrid communications payload made up of 24 C-band, 8 Ku-band and 1 S-band active transponders. The spacecraft will have a 15-year design lifetime and a 5,000 kg launch mass.
After launch, the satellite developed a leakage in the helium pressurization system, which will probably lead to a significant reduction of the operational life.
| Nation: | China |
|---|---|
| Type / Application: | Communication |
| Operator: | China Satcom (formerly Sino Satellite Communications) |
| Contractors: | CAST |
| Equipment: | 24 C-band, 8 Ku-band and 1 S-band active transponders |
| Configuration: | DFH-4 bus |
| Propulsion: | |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | 15 years |
| Mass: | ~ 5000 kg |
| Orbit: | GEO |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| ZX 6A (ChinaSat 6A) (ex Sinosat 6, Xinnuo 6) | 04.09.2010 | Xi LC-2 | CZ-3B/E |
References:
- CAST website
