Details
| Crew Size: | 3 |
|---|---|
| Design Life: | 7 days |
| Orbital Storage: | 200 days |
| Typical orbit: | 223 km x 266 km at 52 degrees inclination |
| Length: | 13.2 m (43.31 ft) |
| Maximum Diameter: | 4.15 m (13.61 ft) |
| Span: | 17.00 m (55.00 ft) |
| Habitable Volume: | 45.00 m3 |
| Mass: | 17,510 kg (38,600 lb) |
| Payload: | 12,600 kg (27,700 lb) |
| Main Engine Thrust: | 7.840 kN (1,763 lbf) |
| Main Engine Propellants: | N2O4/UDMH |
| Main Engine Propellants: | 3,822 kg (8,426 lb) |
| Main Engine Isp: | 291 sec |
| Spacecraft delta v: | 700 m/s (2,290 ft/s) |
| Electrical System: | Solar panels 17 m span 40 m² |
| Electric System: | 2.40 average kW |
| Associated Launch Vehicle: | Proton 8K82K |
Read more about this topic: TKS (spacecraft)
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