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astronautix.com RD-280


Manufacturer Name: RD-280. Designer: Glushko. Developed in: 1963-65. Application: Experimental engine. Propellants: N2O4/Aerozine-50 Thrust(vac): 11,992 kgf. Thrust(vac): 117.60 kN. Isp: 350 sec. Mass Engine: 174 kg. Diameter: 1.3 m. Length: 2.2 m. Chambers: 1. Chamber Pressure: 147.00 bar. Oxidizer to Fuel Ratio: 1.72. Country: Russia. Status: Developed 1963-65. References: 317 . Comments: Experimental engine using Aerozine 50 (50% UDMH + 50% hydrazine) as fuel.
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Last update 12 March 2001.
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