TY - JOUR
T1 - 多模式离子液体推进剂的直流电点火特性研究
AU - Chen, Xucan
AU - Zhuo, Jiankun
AU - Wang, Zun
AU - Gan, Xin
AU - Tang, Yong
AU - Yao, Zhaopu
AU - Li, Shuiqing
AU - Yao, Qiang
N1 - Publisher Copyright:
© 2023 Chinese Academy of Space Technology. All rights reserved.
PY - 2023/12
Y1 - 2023/12
N2 - 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.
AB - 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.
KW - DC electrical ignition
KW - electrical characteristic
KW - electrode material
KW - ionic liquid propellant
KW - voltage response curve
UR - http://www.scopus.com/inward/record.url?scp=85182886752&partnerID=8YFLogxK
U2 - 10.16708/j.cnki.1000-758X.2023.0086
DO - 10.16708/j.cnki.1000-758X.2023.0086
M3 - 文章
AN - SCOPUS:85182886752
SN - 1000-758X
VL - 43
SP - 74
EP - 82
JO - Chinese Space Science and Technology
JF - Chinese Space Science and Technology
IS - 6
ER -