Hydride- and boron-free solid hypergolic H2O2-ignitophores
Hydride- and boron-free solid hypergolic H2O2-ignitophores
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DOI:
10.1016/j.cej.2021.131806
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发表时间:
2021-12
影响因子:
15.1
通讯作者:
Jagadish Das;Daniel Shem-Tov;Shuai-Zhong Wang;Lei Zhang;E. Flaxer;Shi-jie Zhang;Jörg Stierstorfer;Kangcai Wang;Q. Yan;Roman Dobrovetsky;M. Gozin
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文献类型:
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作者:
Jagadish Das;Daniel Shem-Tov;Shuai-Zhong Wang;Lei Zhang;E. Flaxer;Shi-jie Zhang;Jörg Stierstorfer;Kangcai Wang;Q. Yan;Roman Dobrovetsky;M. Gozin
The race and competition in aerospace technologies based on environmentally friendly green propulsion systems with green fuels and oxidizers are attracting a significant attention. Development of hybrid propulsion systems that use a hypergolic fuel and green H2O2oxidizer, capable of deep throttling and restarting from “cold”, is a very challenging task. Here, we describe a new synthetic approach for the synthesis and characterization of conceptually new hydride- and boron-free, and air/moisture stable solid H2O2-hypergols, based on Cu and Co complexes of bis(5-tetrazolyl) amine (H2BTA) ligand. Among prepared and evaluated materials, the best performing compound [K2(H2O)2Cu(BTA)2]n (JD-4) was found to exhibit short ignition delay time of 7 ms (with H2O2, 97%), and high thermostability of 343 °C. Based on obtained ignition results, X-ray crystallography and HASEM software calculations, structure-hypergolic activity-relationship studies were conducted. We found that the electron density difference between Cu and BTA units should be in a specific range (~2) for these compounds to ignite, providing a valuable tool for further development of novel, green, solid fuels for propulsion systems.