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RM-1500H
RM-1500H
RM-1500H
Credit: Boeing / Rocketdyne
Rocketdyne LOx/LH2 rocket engine. Space Shuttle Orbiter Auxiliary Propulsion. Pressure-fed.

Date: 1971. Thrust: 6.66 kN (1,497 lbf). Specific impulse: 400 s.

Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne.
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