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R. W. Marable has written:
'Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle' -- subject(s): RL-10 engines, Specific impulse, Propulsion system performance, Performance tests, Engine tests, Hydrogen oxygen engines, Combustion chambers, Reusable rocket engines, Rocket nozzles, Nozzle design, Rocket engine design, Fabrication
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