Hypergolic propellants based on hydrogen peroxide and organic compounds: historical aspect and current state

被引:33
作者
Guseinov, Sh. L. [1 ]
Fedorov, S. G. [1 ]
Kosykh, V. A. [1 ]
Storozhenko, P. A. [1 ]
机构
[1] State Res Inst Chem & Technol Organoelement Cpds, 38 Shosse Entuziastov, Moscow 105118, Russia
关键词
propellants; hypergol; hydrogen peroxide; IONIC LIQUIDS; HYBRID ROCKET; IGNITION; FUEL; PERFORMANCE; KEROSENE; ENGINE;
D O I
10.1007/s11172-018-2314-1
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
The research towards the development of new propellants aims to ensure not only their high performance, but also high environmental compatibility and low toxicity. Considerable attention is paid to the development of hypergolic propellant compositions, the use of which markedly simplifies the engine design and rocket system operation and provides the possibility of their repeated use. Hydrogen peroxide is a promising and nontoxic oxidant. The review summarizes the research and development data concerning the design and application of hypergolic rocket propellants involving hydrogen peroxide, starting from the 1930s and up to now. The data presented in the review could be useful for specialists engaged in the development of prospective high-performance green fuels.
引用
收藏
页码:1943 / 1954
页数:12
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