RD-182M (original) (raw)
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RD-182M
Glushko LOx/LNG rocket engine. Vozdushnyy Start stage 1. Developed 1998-. Variant of RD-182 engine for liquid natural gas (mainly CH4). Proposed initial candidate for project Vozdushnyy Start of Kompomash.
Status: Developed 1998-. Date: 1998-. Thrust: 882.00 kN (198,281 lbf).
Country: Russia. Propellants: Lox/LNG. Agency: Glushko bureau.
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