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RM-900


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RM-900
Credit: Boeing / Rocketdyne Rocketdyne N2O4/MMH rocket engine. Shuttle Orbiter Reaction Control. Pressure-fed.

Date: 1972. Thrust: 4.00 kN (899 lbf). Specific impulse: 309 s.

Family: Storable liquid. Country: USA. Launch Vehicles: Space Shuttle. 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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