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RD-0229M
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Manufacturer Name: RD-0229M. Designer: Kosberg. Developed in: 1997. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG. Thrust(vac): 883.000 kN (198,506 lbf). Chambers: 1. Country: Russia. Status: Developed 1997. 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.
Bibliography and Further Reading - Polovnikov S P; Karpov, A S, Vestnik Aviatsii i Kosmonavtiki, "Projekt 'Vozdushnyy Start'", Moscow, 1-2/98 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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