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Manufacturer Name: RD-0132. Designer: Kosberg. Developed in: 1996-. Application: upper stage. Propellants: Lox/LH2 Thrust(vac): 10,000 kgf. Thrust(vac): 98.00 kN. Isp: 469 sec. Mass Engine: 370 kg. Length: 1.4 m. Chambers: 4. Chamber Pressure: 98.00 bar. Oxidizer to Fuel Ratio: 5.90. Country: Russia. Status: Design concept 1996-. References: 342 . Comments: Concept for a cryogenic engine for upper stages. Derived from RD-0131, but four chambers with bell nozzles, common turbopump.
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Last update 12 March 2001.
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