Key highlights
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).
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: 2021-02-06
Technical specs
mass
1.01 kg
0.67 kg
0.34 kg
0.67 kg
0.34 kg
propellant type
hydrazine
catalyst
S-405
thrust
85 to 360 N
feed pressure
7 to 35 bar
chamber pressure
4 to 14 bar
expansion ratio
21.5
total thrust pulses
30300
specific impulse
225 to 236 s
total impulse
337620.0 N s
mass flow rate
36.3 to 154.7 g/s
Export
