R-1 stage
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Alcohol propellant rocket stage. Payload 815 / 483 kg. 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.
Related
- Country
- Russia
- Engines
- RD-100
- Propellants
- Lox/Alcohol