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MON/Hydyne
MON/Hydyne propellant. Hydyne (60% UDMH/40% DETA) was a propellant blend pushed rather vigorously by the Redstone arsenal in the late 1950's, but it found little application. No rocket engines went into production using this propellant.

Specific impulse: 335 s. Specific impulse sea level: 287 s.

Optimum Oxidizer to Fuel Ratio: 2.84. Temperature of Combustion: 3,475 deg K. Density: 1.19 g/cc. Oxidizer Density: 1.370 g/cc. Fuel Density: 0.860 g/cc. Fuel Freezing Point: -84 deg C. Fuel Boiling Point: 64 deg C.

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