This page no longer updated from 31 October 2001. Latest version can be found at N1 1962

N1 24 engine version
N1 24 engine version - N1 24 Engine Design of 1962

Credit: © Mark Wade. 2,017 bytes. 97 x 372 pixels.

Family: N. Country: Russia. Status: Study 1962.

Final configuration of N1 at time of development go-ahead. 75 tonne payload selected to support OS-1 heavy space station program.


Liftoff Thrust: 3,459,640 kgf. Total Mass: 2,110,000 kg. Core Diameter: 10.0 m. Total Length: 74.0 m.


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Last update 12 March 2001.
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© Mark Wade, 2001 .