多模式离子液体推进剂的直流电点火特性研究

Translated title of the contribution: DC electrical ignition characteristic of multimode ionic liquid propellant

Xucan Chen, Jiankun Zhuo, Zun Wang, Xin Gan, Yong Tang, Zhaopu Yao, Shuiqing Li*, Qiang Yao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

DC electrical ignition is expected to replace the traditional catalytic combustion for achieving a non-catalytic quick start of ionic liquid propellant due to its capability of rapid ignition. Direct current ignition experiments under atmospheric conditions were carried out for a new multimode hydroxylamine nitrate ( HAN) based ionic liquid propellant. First, the electrical response characteristic of sacrificial electrodes(copper and aluminum)and inert electrodes (stainless steel, platinum, silver, tungsten, molybdenum, and graphite) were tested under different input voltages. The corresponding minimum ignition voltages for different electrode materials were also obtained. Among them, molybdenum and copper electrodes can employ an input voltage of 80 V to ignite the propellant, with a critical electrical response time of less than 1 s. Furthermore,the mechanism of electrochemical reactions was demonstrated when copper was used as a sacrificial electrode by testing various combinations of anode and cathode materials. Finally, high-speed photography was employed to capture the formation and evolution of bubbles during the electrical ignition. It is found that more bubbles were generated on the surface of the anode. After testing the ignition of imidazole-based ionic liquid propellants using eight electrode materials,it can be concluded that the gaseous products were mainly generated near the anode,providing theoretical support for the design of ignition of ionic liquid.

Translated title of the contributionDC electrical ignition characteristic of multimode ionic liquid propellant
Original languageChinese (Traditional)
Pages (from-to)74-82
Number of pages9
JournalChinese Space Science and Technology
Volume43
Issue number6
DOIs
Publication statusPublished - Dec 2023

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