This page no longer updated from 31 October 2001. Latest version can be found at RD-191M

Manufacturer Name: RD-191M . Designer: Glushko. Developed in: 1996-. Application: Angara stage I. Propellants: Lox/Kerosene Thrust(vac): 201,600 kgf. Thrust(vac): 1,976.00 kN. Isp: 338 sec. Chambers: 1. Country: Russia. Status: Developed 1996-. Comments: Single chamber version of the RD-170 / RD-171.
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Last update 12 March 2001.
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© Mark Wade, 2001 .