RD-191M

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RD-191M

Part of RD-170

Glushko LOx/Kerosene rocket engine. Angara stage I. Developed 1996-. Single chamber version of the RD-170 / RD-171.

Status: Developed 1996-. Date: 1996-. Thrust: 1,976.00 kN (444,222 lbf). Specific impulse: 338 s.

Propellant Formulation: Lox/RG-1.

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

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