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RD-0132
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Manufacturer Name: RD-0132. Designer: Kosberg. Developed in: 1996-. Application: upper stage. Propellants: Lox/LH2. Thrust(vac): 98.000 kN (22,031 lbf). Isp: 469 sec. Mass Engine: 370 kg (810 lb). Length: 1.38 m (4.52 ft). Chambers: 4. Chamber Pressure: 98.00 bar. Oxidizer to Fuel Ratio: 5.90. Thrust to Weight Ratio: 27.02. Country: Russia. Status: Design concept 1996-. Concept for a cryogenic engine for upper stages. Derived from RD-0131, but four chambers with bell nozzles, common turbopump.
Bibliography and Further Reading - Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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