RD-56M LNG (original) (raw)

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RD-56M LNG

Part of RD-56

Isayev LOx/LNG rocket engine. Vozdushnyy Start stage 2. Developed 1996-. Variant of RD-56M using liquid natural gas in place of hydrogen. First engine tests performed in 1998.

AKA: KVD-1M LNG. Status: Developed 1996-. Date: 1996-. Thrust: 73.50 kN (16,523 lbf).

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

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