This page no longer updated from 31 October 2001. Latest version can be found at N1F-L3M

N1F - Sr
N1F - Sr - N1F with Sr Lox/LH2 upper stage

5,291 bytes. 79 x 311 pixels.

Family: N. Country: Russia. Status: Cancelled 1971.

The N1M was to be the first Soviet launch vehicle to use liquid oxygen/liquid hydrogen high energy cyrogenic propellants. As originally conceived, the advanced propellants would be used in all upper stages. However this more ambitious work was revised. The first proposed launch vehicle to use such stages would by the N1F, which would have only used the Block S and Block R fourth and fifth stages in place of the N1's Block G and Block D.


Liftoff Thrust: 4,414,910 kgf. Total Mass: 2,773,000 kg. Core Diameter: 10.0 m. Total Length: 104.0 m.


N1M - SrN1M - Sr

4,721 bytes. 79 x 304 pixels.

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Last update 12 March 2001.
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