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並前往https://www.semanticscholar.org/paper/Recent-Developments-in-Rocket-Nozzle-Configurations-Rao/6d49004f17399bef3e7c025d559a125f7f7088c2

[PDF] Recent Developments in Rocket Nozzle Configurations

T THRUST of a rocket engine is primarily dependent upon the momentum imparted to the products of combustion by discharging them through an exhaust nozzle.

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