G-4 stage
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Alcohol propellant rocket stage. Residuals 940 kg. Burnout mass with 3400 kg warhead 7100 kg. Cutoff velocity 4500 m/s, maximum altitude 120 km over 3000 km range. With 10 G limiter thrust would be throttled back and burn time would be 156 seconds.
Related
- Country
- Russia
- Launch Vehicles
- G-4
- Propellants
- Lox/Alcohol