RM-100A RM-100A
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.
Date: 1967. Thrust: 441 N (99 lbf). Specific impulse: 301 s.
Subtopics
RM-100B Rocketdyne Nitric acid/UDMH rocket engine. Satellite Reaction Control. Pressure-fed.
RM-100T Rocketdyne N2O4/Aerozine-50 rocket engine. Lunar Flyer. Pressure-fed.
Family:
Storable liquid.
Country:
USA.
Propellants:
N2O4/MMH.
Agency:
Rocketdyne.
