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Manufacturer Name: RD-0124M. Designer: Kosberg. Developed in: 1998-. Propellants: Lox/Kerosene Thrust(vac): 30,000 kgf. Thrust(vac): 294.30 kN. Isp: 348 sec. Burn time: 300 sec. Mass Engine: 360 kg. Diameter: 1.4 m. Length: 2.1 m. Chambers: 1. Chamber Pressure: 161.90 bar. Country: Russia. Status: Developed 1998-. References: 312 . Comments: Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber.
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Last update 12 March 2001.
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