Specifications | ||
Total Mass | 19,632 kg. | |
Empty Mass | 4,592 kg. | |
Payload | 508 kg. | |
Core Diameter | 1.7 m. | |
Span | 3.6 m. | |
Total Length | 21.0 m. | |
Engines | 1. RD-101 | |
Propellants | Lox/Alcohol | |
Liftoff Thrust | 37,210 kgf. | |
Thrust (vac) | 41,208 kgf. | |
Isp | 237 sec. | |
Isp(sl) | 214 sec. | |
Burn time | 85 sec. | |
Range | 550 km. | |
Maximum altitude | 171 km. | |
Time of flight | 7.5 minutes. | |
Max velocity at burnout | 2175 m/s. | |
Accuracy | 8 km in range, 4 km laterally. |