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RD-0231
Kosberg N2O4/UDMH rocket engine. P-700 Granit. Out of Production. Staged combustion cycle. First flight 1970.

Status: Out of Production. Date: 1968-70. Thrust: 29.00 kN (6,519 lbf). Unfuelled mass: 28 kg (61 lb). Specific impulse: 275 s. Burn time: 16 s. Height: 0.60 m (1.96 ft). Diameter: 0.15 m (0.49 ft).

Engine: 28 kg (61 lb). Chamber Pressure: 123.00 bar. Thrust to Weight Ratio: 105.71.



Family: Storable liquid. Country: Russia. Spacecraft: Granat. Propellants: N2O4/UDMH. Agency: Kosberg bureau. Bibliography: 307.

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