MRE-15/OMV
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
TRW hydrazine monopropellant rocket engine. In Production. Mono-propellant Hydrazine Thrusters.
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.
Related
- Family
- Monopropellant
- Country
- USA
- Agency
- TRW