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Aerojet Rocketdyne has delivered more than 1,500 flight hydrazine monopropellant rocket engines over the past 40 years, and our products cover the full thrust range from 1 N to 4,000 N (0.2 lbf to 900 lbf).


mass1.01 kg
mass0.67 kg
mass0.34 kg
thrustmin: 85 N, max: 360 N
feed pressuremin: 7 bar, max: 35 bar
chamber pressuremin: 4 bar, max: 14 bar
specific impulsemin: 225 s, max: 236 s
total impulse337620.0 N s
mass flow ratemin: 36.3 g s^-1, max: 154.7 g s^-1
full datasheet


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Last updated: 2018-07-13