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N-IFV-II, III - N-IFV-II, III of 1965

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

N-IFV-II, III would use only the first stage from the N-1F, and use new cryogenic second and third stages. This cryogenic second stage seems not to have been pursued beyond the study phase.


LEO Payload: 150,000 kg. to: 220 km Orbit. at: 51.6 degrees. Liftoff Thrust: 5,250,000 kgf. Total Mass: 3,250,000 kg. Core Diameter: 17.0 m. Total Length: 145.0 m.


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Last update 12 March 2001.
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