This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com N1 1962 - V


Gross Mass: 193,000 kg. Empty Mass: 16,000 kg. Thrust (vac): 160,000 kgf. Isp: 347 sec. Burn time: 368 sec. Propellants: Lox/Kerosene Diameter: 4.8 m. Span: 6.8 m. Length: 12.0 m. Country: Russia. No Engines: 4. NK-19 Status: Design 1962. Comments: 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.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .