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MON/Hydrazine
MON/Hydrazine propellant. Mixed Oxides of Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH.

Specific impulse: 343 s. Specific impulse sea level: 295 s.

Optimum Oxidizer to Fuel Ratio: 1.4. Temperature of Combustion: 3,325 deg K. Density: 1.19 g/cc. Oxidizer Density: 1.370 g/cc. Fuel Density: 1.008 g/cc. Fuel Freezing Point: 2.00 deg C. Fuel Boiling Point: 113 deg C.

Subtopics
Dual Mode-Liquid Apogee Engine TRW MON/Hydrazine rocket engine. In Production. First Flight: April 1991. Burn Time 24,000 sec total, with a 3600 sec maximum single burn. Hypergolic ignition via 28 V current to an on/off bi-propellant torque motor valve.
Engines: Dual Mode-Liquid Apogee Engine.
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