MR-103D 1N (0.2-lbf) Rocket Engine Assembly


Summary

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).


Specs

mass0.33 kg
mass0.13 kg
mass0.20 kg
thrustmin: 0.22 N, max: 1.02 N
feed pressuremin: 6.2 bar, max: 27.6 bar
chamber pressuremin: 5.9 bar, max: 23.4 bar
specific impulsemin: 209 s, max: 224 s
total impulse186000 N s
mass flow ratemin: 0.09 g s^-1, max: 0.5 g s^-1
full datasheet

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Last updated: 2018-07-13