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Engine Model: DMT-600. Designer: Isayev. Propellants: N2O4/UDMH. Thrust(vac): 600 N (130 lbf). Isp: 301 sec. Burn time: 5,000 sec. Mass Engine: 4.20 kg (9.20 lb). Chambers: 1. Chamber Pressure: 9.00 bar. Area Ratio: 46.50. Oxidizer to Fuel Ratio: 1.85. Thrust to Weight Ratio: 14.52. Country: Russia. Status: In Production.

Bi-propellant hypergolic (self-igniting) engine, pressure-fed. 6,000 ignitions

Bibliography:

  • Haeseler, Dietrich, Visit to the museum of Chemical Machining Design Bureau, Kalinin 1998 via Dietrich Haeseler.
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