MR-103G 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
mass0.127 kg
mass0.204 kg
thrustmin: 0.19 N, max: 1.13 N
feed pressuremin: 4.8 bar, max: 28.3 bar
chamber pressuremin: 4.5 bar, max: 23.8 bar
specific impulsemin: 202 s, max: 224 s
total impulse97078 N s
mass flow ratemin: 0.09 g s^-1, max: 0.5 g s^-1
full datasheet

RFQ/RFI

Submitting your information allows us to get in touch with you once we get a response from the supplier.

I am interested in*:

Add any additional comments that pertain to your request. The more context you can provide, the faster we'll be able to get you the information that you want.


Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.

Last updated: 2018-07-13