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RD-280
Glushko N2O4/Aerozine-50 rocket engine. Experimental engine. Study 1961. Experimental engine using Aerozine 50 (50% UDMH + 50% hydrazine) as fuel.

Status: Study 1961. Date: 1963-65. Thrust: 117.60 kN (26,438 lbf). Unfuelled mass: 174 kg (383 lb). Specific impulse: 350 s. Height: 2.20 m (7.20 ft). Diameter: 1.27 m (4.15 ft).

Engine: 174 kg (383 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 68.91. Oxidizer to Fuel Ratio: 1.718.

Subtopics
8D725 Glushko N2O4/UDMH rocket engine. Developed 1963-1970. 10 to 12 metric ton thrust engine developed for an unstated military requirement.
Family: Storable liquid. Country: Russia. Propellants: N2O4/Aerozine-50. Stages: R-56 Block K. Agency: Glushko bureau. Bibliography: 317.
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