This page no longer updated from 31 October 2001.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

astronautix.com 11D52M


Government Designation: 11D52M. Designer: Kuznetsov. Developed in: 1965. Application: N1M 1965 - B. Used on stages: N1M 1965 - B. Used on launch vehicles: N-IM 1965, N-IMV-III. Propellants: Lox/Kerosene Thrust(vac): 280,000 kgf. Thrust(vac): 2,745.00 kN. Isp: 330 sec. Isp (sea level): 296 sec. Chambers: 1. Country: Russia. Status: Design concept 1965. References: 283 . Comments: As per N1 improvement study, 1965. Thrust increased to 280 tonnes per engine.
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 .