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Towards Safer Rocket Fuels: Hypergolic Imidazolylidene‐Borane Compounds as Replacements for Hydrazine Derivatives
Author(s) -
Huang Shi,
Qi Xiujuan,
Liu Tianlin,
Wang Kangcai,
Zhang Wenquan,
Li Jianlin,
Zhang Qinghua
Publication year - 2016
Publication title -
chemistry – a european journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.687
H-Index - 242
eISSN - 1521-3765
pISSN - 0947-6539
DOI - 10.1002/chem.201601343
Subject(s) - hydrazine (antidepressant) , chemistry , ammonia borane , specific impulse , fire retardant , combustion , borane , ignition system , propellant , organic chemistry , aerospace engineering , hydrogen , catalysis , hydrogen storage , biochemistry , engineering
Currently, toxic and volatile hydrazine derivatives are still the main fuel choices for liquid bipropellants, especially in some traditional rocket propulsion systems. Therefore, the search for safer hypergolic fuels as replacements for hydrazine derivatives has been one of the most challenging tasks. In this study, six imidazolylidene‐borane compounds with zwitterionic structure have been synthesized and characterized, and their hypergolic reactivity has been studied. As expected, these compounds exhibited fast spontaneous combustion upon contact with white fuming nitric acid (WFNA). Among them, compound 5 showed excellent integrated properties including wide liquid operating range (−70–160 °C), superior loading density (0.99 g cm −3 ), ultrafast ignition delay times with WFNA (15 ms), and high specific impulse (303.5 s), suggesting promising application potential as safer hypergolic fuels in liquid bipropellant formulations.