This page no longer updated from 31 October 2001. Latest version can be found at RD-0229M

Manufacturer Name: RD-0229M. Designer: Kosberg. Developed in: 1997. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG Thrust(vac): 90,000 kgf. Thrust(vac): 883.00 kN. Chambers: 1. Country: Russia. Status: Developed 1997. References: 327 . Comments: Derivative of RD-0229 for the propellants LOX and liquid natural gas (methane). Initial candidate for stage 1 propulsion of Vozdushnyy Start project by Kompomash.
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 .