This page no longer updated from 31 October 2001.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

astronautix.com N1 Nuclear AF


Family: N. Country: Russian. Status: Study 1963.

A variant of the first alternative considered in the 1962 nuclear N1 study. This was a 'high thrust' version of the Type A engine - apparently with higher propellant rate, lower specific impulse, and lower engine weight. Due to the very low density of the enormous liquid hydrogen upper stages, these immense vehicles would have been very ungainly (and had interesting stress problems during ascent!)


Specifications

LEO Payload: 300,000 kg. to: 220 km Orbit. at: 51.6 degrees. Payload: 27,100 kg. to a: lunar surface trajectory. Liftoff Thrust: 3,600,000 kgf. Total Mass: 2,500,000 kg. Core Diameter: 17.0 m. Total Length: 200.0 m.


N1 Nuclear AF Chronology


- 1963 May -

Bibliography:



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .