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Manufacturer Name: RD-0124M1. Designer: Kosberg. Developed in: 1998-. Propellants: Lox/Kerosene Thrust(vac): 30,000 kgf. Thrust(vac): 294.30 kN. Isp: 359 sec. Burn time: 300 sec. Mass Engine: 393 kg. Diameter: 1.5 m. Length: 2.6 m. Chambers: 1. Chamber Pressure: 157.00 bar. Country: Russia. Status: Developed 1998-. References: 312 . Comments: Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber with larger nozzle extension compared to RD-0124M.
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Last update 12 March 2001.
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