This page no longer updated from 31 October 2001. Latest version can be found at N-IFV-III

N1FV-III - N-IFV-III design of 1965

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Family: N. Country: Russia. Status: Study 1965.

Then N-IFV-III would add the Block V-III cryogenic third stage to the first and second stages of the N-IF.


LEO Payload: 125,000 kg. to: 220 km Orbit. at: 51.6 degrees. Liftoff Thrust: 5,250,000 kgf. Total Mass: 3,000,000 kg. Core Diameter: 17.0 m. Total Length: 125.0 m.


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Last update 12 March 2001.
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