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MRE-15/OMV
Part of MRE engine series Family
TRW hydrazine monopropellant rocket engine. In Production. Mono-propellant Hydrazine Thrusters.

Status: In Production. Thrust: 89 N (20 lbf). Unfuelled mass: 1.13 kg (2.49 lb). Specific impulse: 225 s. Burn time: 2,000 s. Height: 0.27 m (0.88 ft).

Mass: 1.13 kg. Length: 26.9 cm. Engine Cycle: decomposition of hydrazine over heated shell catalyst. Thrust: 44.5-89 N in vacuum. Isp: 225 sec in vacuum at steady state conditions. Inlet Pressure: 12-27 atm. Burn Time: 0.020 sec. Total Cycles: 100,000.

Engine: 1.13 kg (2.49 lb). Chamber Pressure: 27.00 bar. Thrust to Weight Ratio: 7.96.



Family: Monopropellant. Country: USA. Agency: TRW.

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