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    • 1. 发明授权
    • Liquid-solid propulsion system and method
    • 液固推进系统及方法
    • US5099645A
    • 1992-03-31
    • US541862
    • 1990-06-21
    • Alan L. SchulerDanny R. Wiley
    • Alan L. SchulerDanny R. Wiley
    • B64G1/40C06B47/06F02K9/50F02K9/72
    • C06B47/06B64G1/402B64G1/404F02K9/50F02K9/72
    • A liquid-solid propulsion system having a tank of liquid oxygen and a high pressure chamber loaded with solid grain fuel with a portion of the liquid oxygen being passed through a heat exchanger to convert the liquid oxygen to gaseous oxygen. The gaseous oxygen is directed to the chamber or solid grain fuel to induce a fuel rich gas burn that is directed to a thrust chamber which also receives liquid oxygen to increase the characteristic velocity of the exhaust and thereby provide the specific impulse of the propulsion system. The gaseous oxygen is also directed to the liquid oxygen tank to pressurize the flow of liquid oxygen from the tank. Valves are interposed to control the flow of liquid and gaseous oxygen to provide the required mixture ratio in the thrust chamber for optimum specific impulse or to terminate the thrust of the propulsion system. A method for providing the liquid-solid propulsion system is also disclosed.
    • 具有液氧罐的液固推进系统和装有固体颗粒燃料的高压室,一部分液氧通过热交换器以将液氧氧化成气态氧。 气态氧被引导到室或固体颗粒燃料以引起燃料丰富的气体燃烧,其引导到推进室,其还接收液体氧以增加排气的特征速度,从而提供推进系统的比冲量。 气态氧也被引导到液氧罐以对来自罐的液氧流进行加压。 插入阀以控制液体和气态氧的流动,以在推力室中提供所需的混合比,以获得最佳比冲量或终止推进系统的推力。 还公开了一种用于提供液固推进系统的方法。