RD-120.03

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RD-120.03

Part of RD-120

Glushko LOx/Kerosene rocket engine. Design concept.

Status: Design concept. Thrust: 882.00 kN (198,281 lbf). Specific impulse: 353 s.

Country: Russia. Propellants: Lox/Kerosene. Agency: Glushko bureau.

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