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RS-52
RS-52
RS-52
Credit: Boeing / Rocketdyne
Rocketdyne LOx/LH2 rocket engine. Oxygen/Hydrogen Space Station Thruster. Pressure-fed. Technology was developed with 0.1 lb thrust resistojet by using electrically heated waste for space station propulsion.

Date: 1983. Thrust: 107 N (24 lbf). Specific impulse: 405 s.



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

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