Invention Grant
US07815146B2 Combustible outgassing material lined altitude compensating rocket nozzle 有权
可燃除气材料内衬高度补偿火箭喷嘴

Combustible outgassing material lined altitude compensating rocket nozzle
Abstract:
A fixed sized bell rocket nozzle is lined with a layer of combustible material that is ignited during launch ignition and burns to outgas into the rocket exhaust for spatially variably confining the exhaust and perfecting an effective variably sized altitude compensating exhaust nozzle that maximizes lift during the launch of a spacecraft into orbit.
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