N1 1962 - V
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Compared to total fuelled mass excludes 1,000 kg in propellants lost to boil-off prior to stage ignition. Values as in draft project as defended on 2-16 July 1962.
No Engines: 4.
Related
- Country
- Russia
- Engines
- NK-19
- Launch Vehicles
- N1 1962
- Propellants
- Lox/Kerosene