A detailed mechanism for the initial hypergolic reaction in liquid hydrazine/nitrogen tetroxide mixtures based on quantum chemistry calculations
A detailed mechanism for the initial hypergolic reaction in liquid hydrazine/nitrogen tetroxide mixtures based on quantum chemistry calculations
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DOI:
10.1016/j.combustflame.2021.02.035
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发表时间:
2021-07
影响因子:
4.4
通讯作者:
Y. Izato;K. Shiota;A. Miyake
中科院分区:
文献类型:
--
作者:
Y. Izato;K. Shiota;A. Miyake
This work determined a chemical mechanism for the early stage of hypergolic ignition following contact between hydrazine (N2H4) and nitrogen tetroxide (N2O4), both in the liquid state. Such mixtures have been used in thrusters for spacecraft applications for many years, and the effective development and use of such propellants requires an understanding of their detonation-like ignition under various conditions. Liquid-phase reactions were investigated using quantum chemical calculations at the CBS-QB3//ωB97X-D/SMD level of theory, and the results showed that the energy barrier to the reaction N2H4+ N2O4→ NH2NHNO2+ HNO2was much lower than values predicted for the same reaction in the gas phase. Based on these results, a detailed kinetic model for the liquid-phase reaction was constructed and employed to predict the temperature increase obtained from N2H4/N2O4propellants under pre-mixed and adiabatic conditions. The time to reach the N2H4boiling point of 114 °C was estimated at approximately 0.06 μs, which explains the rapid formation of a vapor phase in previous droplet pool tests. Analyses of the rate of production and the temperature sensitivity established that the N2H4+ N2O4→ NH2NHNO2+ HNO2step plays the most important role in triggering a series of subsequent reactions, and thus determines the rate of temperature rise.