DST-100 (original) (raw)

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DST-100

Part of DST engine series

Isayev N2O4/UDMH rocket engine. In Production. Bi-propellant hypergolic (self-igniting) engine, pressure-fed. 10,000 ignitions

Status: In Production. Thrust: 100 N (20 lbf). Unfuelled mass: 1.10 kg (2.40 lb). Specific impulse: 276 s. Burn time: 10,000 s.

Engine: 1.10 kg (2.40 lb). Chamber Pressure: 15.00 bar. Area Ratio: 43. Thrust to Weight Ratio: 9.09. Oxidizer to Fuel Ratio: 1.85.

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

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