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Improvements in jet propulsion units, more particularly rockets, and in methods of producing hot gases for the propulsion thereof

机译:改进喷气推进装置,特别是火箭,以及产生用于推进其的热气体的方法

摘要

A rocket or jet propulsion unit is operated with the aid of a fuel comprising molten lithium, which is injected into the central zone of the combustion chamber and reacted therein with an oxidizing agent, an auxiliary fuel of lower combustion temperature being simultaneously injected into the combustion chamber and reacted with an oxidizing agent so that the central zone of the chamber is separated from the wall of the chamber by a peripheral zone where the lower temperature combustion reaction takes place. The melting point of the lithium may be reduced by alloying it with small quantities of sodium and potassium. The auxiliary fuel may be kerosene; hydrazine or an aromatic amine such as xylidine. The molten lithium and the auxiliary fuel may be reacted with the same oxidizing agent or different oxidizing agents may be used for the two fuels. Examples of suitable oxidizing agents are nitric acid and fuming nitric acid.
机译:火箭或喷气推进装置借助含熔融锂的燃料运行,该燃料被注入燃烧室的中心区域并在其中与氧化剂反应,同时将燃烧温度较低的辅助燃料注入燃烧室。室与氧化剂反应,使得室的中心区域被发生低温燃烧反应的周边区域与室壁隔开。可以通过将锂与少量钠和钾合金化来降低其熔点。辅助燃料可以是煤油。肼或芳族胺,例如二甲苯胺。熔融锂和辅助燃料可以与相同的氧化剂反应,或者可以将不同的氧化剂用于两种燃料。合适的氧化剂的例子是硝酸和发烟硝酸。

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