This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com N1F

N1F - 1974
N1F - 1974 - N1F - 1974 Configuration (N1 s/n 8L)

5,494 bytes. 79 x 366 pixels.



Family: N. Country: Russia. Status: Cancelled 1974.

The N1F would have been the definitive flight version of the N1, incorporating all changes resulting from the four flight tests of the vehicle, including the new Kuznetsov engines and 10% greater liftoff mass by using superchilled propellants in all stages. N1 8L would have been the first N1F configuration flight, with launch planned in the third quarter of 1975 at the time the project was cancelled.


Specifications

LEO Payload: 105,000 kg. to: 220 km Orbit. at: 51.6 degrees. Liftoff Thrust: 4,530,000 kgf. Total Mass: 3,025,000 kg. Core Diameter: 17.0 m. Total Length: 105.0 m.


N1F Chronology


- 1970 June -
1972 Feb 16 -
1972 Feb 23 -
1972 May 15 -
1974 May 2 -
1974 May 19 -
1974 Jun 24 -
1976 Feb 17 -

Bibliography:



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .