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DST-25
Part of DST engine series Family
Isayev N2O4/UDMH rocket engine. In Production. Bi-propellant hypergolic (self-igniting) engine, pressure-fed. 300,000 ignitions

Status: In Production. Thrust: 25 N (5 lbf). Unfuelled mass: 0.90 kg (1.98 lb). Specific impulse: 285 s. Burn time: 25,000 s.

Engine: 0.90 kg (1.98 lb). Chamber Pressure: 8.00 bar. Area Ratio: 45. Thrust to Weight Ratio: 2.83. Oxidizer to Fuel Ratio: 1.85.



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

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