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astronautix.com 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.
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Last update 12 March 2001.
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