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RM-100A


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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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