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DST-200
Part of DST engine series Family
Isayev N2O4/UDMH rocket engine. In Production. Bi-propellant hypergolic (self-igniting) engine, pressure-fed. 10,000 ignitions

Status: In Production. Thrust: 200 N (40 lbf). Unfuelled mass: 1.30 kg (2.80 lb). Specific impulse: 280 s. Burn time: 5,000 s.

Engine: 1.30 kg (2.80 lb). Chamber Pressure: 15.00 bar. Area Ratio: 43. Thrust to Weight Ratio: 15.38. Oxidizer to Fuel Ratio: 1.85.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Isayev bureau. Bibliography: 350.

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