DST-100A

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DST-100A

Part of DST engine series

Isayev N2O4/UDMH rocket engine. In Production. Bi-propellant hypergolic engine, pressure-fed. Larger nozzle and reduced chamber pressure to increase performance and lifetime in comparison to DST-100. 450,0000 ignitions.

Status: In Production. Thrust: 100 N (20 lbf). Unfuelled mass: 1.50 kg (3.30 lb). Specific impulse: 304 s. Burn time: 50,000 s.

Engine: 1.50 kg (3.30 lb). Chamber Pressure: 7.70 bar. Area Ratio: 100. Thrust to Weight Ratio: 6.66. Oxidizer to Fuel Ratio: 1.85.

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

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