R-2 stage
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Alcohol propellant rocket stage. Payload 1350 / 508 kg. 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.
Related
- Country
- Russia
- Engines
- RD-101
- Propellants
- Lox/Alcohol