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Distributed erosion region rocket motor nozzle
Distributed erosion region rocket motor nozzle
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机译:分布式腐蚀区火箭发动机喷嘴
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摘要
A rocket motor nozzle has a nozzle core that defines a nozzle passage through which combustion products travel during flight. The erosive forces created by the combustion products are longitudinally distributed over the nozzle core so that the nozzle's smallest area remains substantially constant in spite of the erosion. An inner surface of the nozzle core defines the nozzle passage. The inner surface includes an entry region which defines a nozzle entry, an exit region which defines an exit, and an elongate erosion region which defines an erosion passage between the entry and exit. The erosion region length is greater than the average smallest passage diameter, thereby allowing the location of the erosion focus along the erosion region to vary over time as a result of erosion of the erosion region. The nozzle core is formed of a fibrous composite material which is selected according to the type of propellant used and which includes fibers oriented transverse to the erosion passage to resist erosion.
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