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RD-0124M
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Manufacturer Name: RD-0124M. Designer: Kosberg. Developed in: 1998-. Propellants: Lox/Kerosene. Thrust(vac): 294.300 kN (66,161 lbf). Isp: 348 sec. Burn time: 300 sec. Mass Engine: 360 kg (790 lb). Diameter: 1.43 m (4.69 ft). Length: 2.10 m (6.80 ft). Chambers: 1. Chamber Pressure: 161.90 bar. Thrust to Weight Ratio: 83.33. Country: Russia. Status: Developed 1998-. Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber.
Bibliography and Further Reading - Haeseler, Dietrich, CADB-information leaflets, International Aerospace Show Berlin 1998 (ILA 98) via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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