This page no longer updated from 31 October 2001. Latest version can be found at NK-9

Manufacturer Name: NK-9. Designer: Kuznetsov. Developed in: 1959-65. Application: R-9, GR-1 stage 1. Used on stages: GR-1 Stage 1, Superraket Block A. Used on launch vehicles: GR-1, Superraket. Propellants: Lox/Kerosene Thrust(vac): 45,000 kgf. Thrust(vac): 441.30 kN. Isp: 327 sec. Isp (sea level): 280 sec. Chambers: 1. Country: Russia. Status: Out of Production. First Flight: 1965. References: 283 , 306 , 319 . Comments: Developed for 1st Stage of the R-9 ICBM, reached phase of stand testing, but then RD-111 selected. Later planned for 1st Stage of GR-1, but that rocket was abandoned. OKB Kuznetsov.
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 .