Aerojet N2O4/MMH rocket engine. 0.021 kN. In Production. Mixture Ratio(O/F): 1.60. Isp=285s.
Engine: 0.57 kg (1.25 lb). Area Ratio: 75. Thrust to Weight Ratio: 3.81.
Status: In Production.
More... - Chronology...
Unfuelled mass: 0.57 kg (1.25 lb).
Thrust: 21 N (5 lbf).
Specific impulse: 285 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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