RD-0229M

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RD-0229M

Part of RD-0228

Kosberg LOx/LNG rocket engine. Vozdushnyy Start stage 1. 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.

Status: Developed 1997. Date: 1997. Thrust: 883.00 kN (198,506 lbf).

Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau.

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