N1 1962 - A
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
NK-15 / 11D51 rocket engine for first stage of N1
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Earlier design for the Block A. Includes 14,000 kg for Stage 1-2 interstage and payload fairing. Compared to total fuelled mass excludes 15,000 kg propellant expended in thrust build-up and boil-off prior to liftoff. Values as in draft project as defended on 2-16 July 1962.
No Engines: 24.
Related
- Country
- Russia
- Engines
- NK-15
- Launch Vehicles
- N1 Nuclear A, N1 Nuclear V-B, N1 Nuclear AF, N1 Nuclear V, N1 1962
- Propellants
- Lox/Kerosene
Photo Gallery
NK15 engine
NK-15 / 11D51 rocket engine for first stage of N1
Credit: © Mark Wade
