This page no longer updated from 31 October 2001.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

astronautix.com N1-MOK

N1 MOK
N1 MOK -

4,559 bytes. 97 x 184 pixels.



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

Ultimate derivative of N1. Single-stage-to-orbit vehicle based on N1 Block A. Propellants changed to LH2/LOX, 16 x modified NK-33 engines + 4 Liquid Air Cycle Engine Liquid Air/LH2 boosters. All figures estimated based on tank volume of Block A and delivery of 90,000 kg payload to 450 km / 97.5 degree MKBS orbit. Briefly described in RKK Energia official history and in some detail in Peter James'

book Soviet Conquest from Space!
Specifications

Liftoff Thrust: 3,255,810 kgf. Total Mass: 1,200,000 kg. Core Diameter: 10.0 m. Total Length: 36.0 m.



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 .