RD-120.01

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RD-120.01

Part of RD-120

Glushko LOx/Kerosene rocket engine. Design concept.

Status: Design concept. Thrust: 784.00 kN (176,250 lbf). Specific impulse: 329 s.

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

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