Specifications | ||
Total Mass | 12,798 kg. | |
Empty Mass | 4,066 kg. | |
Payload | 483 kg. | |
Core Diameter | 1.7 m. | |
Span | 3.6 m. | |
Total Length | 17.0 m. | |
Engines | 1. RD-100 | |
Propellants | Lox/Alcohol | |
Liftoff Thrust | 27,690 kgf. | |
Thrust (vac) | 31,314 kgf. | |
Isp | 233 sec. | |
Burn time | 63 sec. | |
Isp(sl) | 206 sec. | |
Diameter | 1.7 m. | |
Range | 270 km. | |
Maximum altitude | 77 km. | |
Time of flight | 5 minutes. | |
Max velocity at burnout | 1465 m/s. | |
Accuracy | 8 km in range, 4 km laterally. |