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RS-52 -

Credit: Boeing / Rocketdyne. 6,555 bytes. 167 x 174 pixels.

Manufacturer Name: RS-52. Designer: Rocketdyne. Developed in: 1983. Propellants: Lox/LH2 Thrust(vac): 11 kgf. Isp: 405 sec. Comments: 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .