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astronautix.com 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.


Specifications

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



Bibliography:



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