N1 Block G
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Empty mass estimated.
Subtopics
- N-11 1963 - V LOx/Kerosene propellant rocket stage. Conjectural stage derived from GR-1 stage 1 to match total mass given of launch vehicle.
- GR-1 Stage 1 LOx/Kerosene propellant rocket stage. Payload 4,000 kg (2.2 MT nuclear warhead). Range 13,000 km or orbital. Accuracy (90%) 5 km in range and 3 km in dispersion. Masses estimated based on total vehicle mass of 117 metric tons.
Related
- Country
- Russia
- Engines
- NK-19
- Propellants
- Lox/Kerosene