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


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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.

作者简介

Sh. Guseinov

State Research Institute for Chemistry and Technology of Organoelement Compounds 38 shosse Entuziastov

编辑信件的主要联系方式.
Email: stan-fed2011@yandex.ru
俄罗斯联邦, Moscow, 105118

S. Fedorov

State Research Institute for Chemistry and Technology of Organoelement Compounds 38 shosse Entuziastov

Email: stan-fed2011@yandex.ru
俄罗斯联邦, Moscow, 105118

V. Kosykh

State Research Institute for Chemistry and Technology of Organoelement Compounds 38 shosse Entuziastov

Email: stan-fed2011@yandex.ru
俄罗斯联邦, Moscow, 105118

P. Storozhenko

State Research Institute for Chemistry and Technology of Organoelement Compounds 38 shosse Entuziastov

Email: stan-fed2011@yandex.ru
俄罗斯联邦, Moscow, 105118


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