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Propulsion for rocket used to launch low-orbit satellites
Propulsion for rocket used to launch low-orbit satellites
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机译:用于发射低轨道卫星的火箭推进
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摘要
The rocket motor has a gas ejection nozzle (1) and a chamber (5) for injection of a propulsive fluid. An induction loop (8) is wrapped round part (4) of the nozzle. A high frequency electric generator (11) supplies this coil. The propulsive fluid is preheated by being used as a coolant for the generator.
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