This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 1,942,000 kg.
Empty Mass: 192,000 kg. Thrust (vac): 5,040,000 kgf. Isp: 331 sec. Burn time: 113 sec. Propellants: Lox/Kerosene Isp(sl): 296 sec. Diameter: 10.0 m. Span: 17.0 m. Length: 30.0 m. Country: Russia. No Engines: 30. NK-15 Status: Design 1964. Comments: As per draft project for N1-L3, 1964. Block A modified with six additional engines and propellant increased by 550 tonnes by using chilled propellants.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .