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astronautix.com RD-182M


Manufacturer Name: RD-182M. Designer: Glushko. Developed in: 1998-. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG Thrust(vac): 89,940 kgf. Thrust(vac): 882.00 kN. Chambers: 1. Country: Russia. Status: Developed 1998-. References: 327 . Comments: Variant of RD-182 engine for liquid natural gas (mainly CH4). Proposed initial candidate for project Vozdushnyy Start of Kompomash.
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Last update 12 March 2001.
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