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RD-0122
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Manufacturer Name: RD-0122. Designer: Kosberg. Developed in: 1990-. Application: Energia-M core stage. Planned for Angara central stage. Propellants: Lox/LH2. Thrust(vac): 2,313.000 kN (519,983 lbf). Isp: 461 sec. Chambers: 1. Country: Russia. Status: Developed 1990-. Based on RD-0120. Upgrade of RD-0120 engine for Energia-M launcher with increased thrust. Prototype from RD-0120 hardware. Later an upgraded RD-0122 was planned for use in the central stage of an early version of the Angara heavy launcher.
Bibliography and Further Reading - Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
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