Aerojet N2O4/MMH rocket engine. 0.445 kN. In Production. Mixture Ratio(O/F): 1.65. Isp=309s.
Engine: 1.86 kg (4.10 lb). Area Ratio: 150. Thrust to Weight Ratio: 24.39.
Status: In Production.
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Unfuelled mass: 1.86 kg (4.10 lb).
Thrust: 445 N (100 lbf).
Specific impulse: 309 s.
Associated Manufacturers and Agencies
Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
N2O4/MMH Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Monomethylhydrazine (CH3NHNH2) is a storable liquid fuel that found favour in the United States for use in orbital spacecraft engines. Its advantages in comparison to UDMH are higher density and slightly higher performance. More...
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