On the Delay Time of Induced Electrostatic Discharge of Metal Electrode under the Action of ESD EMP

doi:10.3969/j.issn.1000-1093.2021.11.014

Abstract

Abstract: For the problem about electrostatic discharge induced by strength electromagnetic field, the delay time of electrostatic discharge of metal electrode is studied to further explore the changing law of its electrostatic discharge under the action of strong electromagnetic field. The electrostatic discharge rule of metal electrode under the action of strong electromagnetic field is emphatically analyzed from the formation process of discharge channel and the mechanism of electrostatic discharge induced by electromagnetic field. The test results show that enhancement in the magniude of radiated field strnegth results in the shorted delay time of induced discharge under the action of strong electromagnetic pulse radiation field, and the voltage between metal electrodes and the air pressure all have impact on the delay time of induced discharge under the action of strong electromagnetic pulse. The delay time of induced discharge gradually shortens and the dispersion of time delay also becomes gradually smaller with the increase in metal electrode voltage, radiated field strength or air pressure.

Key words: strongelectromagneticfield, electrostaticdischarge, strongelectromagneticpulseradiation, induction, delaytime

CLC Number:

TM151⁺.1

ZHANG Jianping, HU Xiaofeng, LIU Shanghe, WEI Ming. On the Delay Time of Induced Electrostatic Discharge of Metal Electrode under the Action of ESD EMP[J]. Acta Armamentarii, 2021, 42(11): 2409-2417.

References

［1］吴汉基, 蒋远大,张志远,等．航天器表面电位的主动控制［J］. 中国航天, 2008(6): 36-40.
WU H J, JIANG Y D, ZHANG Z Y, et al. Active control of spacecraft surface potential ［J］. Aerospace China, 2008(6): 36-40. (in Chinese)
［2］ FENG W Q. Ground simulation test of large space geomagnetic sub-storm environment ［J］. Spacecraft Environmental Engineering, 2001, 18(4): 33-42.
［3］胡小锋,张建平,许滨.航天器空间静电效应研究进展［J］.强激光与粒子束,2019,31(10): 6-14.
HU X F, ZHANG J P, XU B. Progress of the research of space electrostatic effect of spacecraft ［J］. High Power Laser and Particle Beam, 2019,31(10): 6-14.（in Chines）
［4］朱长青，刘尚合，魏明. ESD辐射场测试研究［J］. 电子学报，2005，33(9)：1702-1705.
ZHU C Q, LIU S H, WEI M. A study on test & measurement of radiated field by ESD ［J］. Acta Electronica Sinica, 2005, 33(9): 1702-1705.
［5］刘尚合, 胡小锋, 原青云,等. 航天器充放电效应与防护研究进展［J］. 高电压技术, 2019, 45(7):2108-2118.
LIU S H, HU X F, YUAN Q Y, et al. Research progress in charging-discharging effects and protection of spacecraft ［J］. High Voltage Engineering, 2019, 45(7):2108-2118.(in Chinese)
［6］ WRIGHT K H, SCHNEIDER T A, VAUGHN J A, et al. Electrostatic discharge testing of multijunction solar array coupons after combined space environmental exposures［J］. IEEE Transactions on Plasma Science, 2012, 40(2): 334-344.
［7］许滨，原青云，武占成，等. 低气压环境下航天材料静电防护地面模拟［J］. 高电压技术，2013，39(12)：2894-2898.
XU B, YUAN Q Y, WU Z C, et al. Protection against of electrostatic charge of aerospace material in low pressure environment developed through round simulation［J］. High Voltage Engineering, 2013, 39(12): 2894-2898.(in Chinese)
［8］原青云，孙永卫，张希军，等. 航天器带电理论及防护［M］. 北京: 国防工业出版社，2016.
YUAN Q Y, SUN Y W, ZHANG X J, et al. Electrification theory and protection of spacecraft ［M］. Beijing: National Defense Industry Press, 2016.(in Chinese)
［9］ ABDEL-AZIZ Y A, EL-HAMEED A M A. Ground-based simulation for the effects of space plasma on spacecraft［J］. Advances in Space Research, 2013, 51(1): 133-142.
［10］ LAI S T. Fundamentals of spacecraft charging: spacecraft interactions with space plasma［M］. Princeton, NJ, US: Princeton University Press, 2012.
［11］赵呈选，李得天，杨生胜，等. 低地球轨道航天器表面充电及其环境影响因素［J］. 高电压技术，2017，43(5)：1438-1444．
ZHAO C X, LI D T, YANG S S, et al. Surface charging and its environment influencing factors for low earth orbit spacecraft［J］. High Voltage Engineering, 2017, 43(5): 1438-1444.(in Chinese)
［12］刘尚合，魏光辉，刘直承. 静电理论与防护［M］. 北京：兵器工业出版社，1999．
LIU S H, WEI G H, LIU Z C. Electrostatic theory and protection［M］. Beijing: Publishing House of Ordnance Industry， 1999.(in Chinese)
［13］刘业楠，赵华，易忠，等．空间站带电效应分析及对策［J］．载人航天，2013：19(5):6-12.
LIU Y N, ZHAO H, YI Z, et al. Analysis and Countermeasures of charging effects in space station ［J］. Manned Spaceflight, 2013:19(5): 6-12.
［14］谢喜宁, 胡小锋, 原青云. 静电电磁脉冲辐射场诱发针-球电极结构放电试验［J］. 航空学报, 2019, 40(11): 323161.
XIE X N, HU X F, YUAN Q Y. Electrostatic electromagnetic pulse radiation field induced needle-sphere electrode structural discharge test ［J］. Acta Aeronautica et Astronautica Sinica, 2019, 40(11): 323161.(in Chinese)
［15］ LAI S T．航天器带电原理——航天器与空间等离子体的相互作用［M］．李盛涛，郑晓泉，陈玉，等，译．北京：科学出版社，2015.
LAI S T. Principle of spacecraft electrification-interaction between spacecraft and space plasma ［M］. LI S T, ZHENG X Q, CHEN Y, et al, translated. Beijing: Science Press, 2015．(in Chinese)
［16］全荣辉，韩建伟，黄建国，等．电介质材料辐射感应电导率的模型研究［J］．物理学报，2007,56(11):6642-6647．
QUAN R H, HAN J W, HUANG J G, et al. Modeling analysis of radiation induced conductivity in electrical insulator ［J］. Acta Physica Sinica, 2007,56(11): 6642-6647.(in Chinese)
［17］薛梅．高压砷化镓太阳阵ESD效应及防护技术研究［D］．天津：天津大学，2007．
XUE M. Research on ESD effect and protection technology of high pressure GaAs solar array ［D］. Tianjin: Tianjin University, 2007.

［18］黄本诚，童靖宇．空间环境工程学［M］．北京：中国科学技术出版社，2010．
HUANG B C, TONG J Y. Space environmental engineering ［M］. Beijing: China Science and Technology Press, 2010.
［19］胡小锋，刘尚合，王雷，等．尖端导体电晕放电辐射场的计算与实验［J］．高电压技术，2012,38(9):2266-2272．
HU X F, LIU S H, WANG L, et al. Calculation and experiment of radiation fields from from tip corona discharge ［J］. High Voltage Engineering, 2012,38(9): 2266-2272.(in Chinese)
［20］曹鹤飞，马策一，刘浩，等．电磁场辐照诱发真空电晕放电模拟试验系统［J］．强激光与粒子束，2016,28(8):112-115．
CAO H F, MA C Y, LIU H, et al. Simulation test system of vacuum corona discharge induced by electromagnetic field ［J］. High Power Laser and Particle Beams, 2016,28(8): 112-115.(in Chinese)
［21］唐旭,季启政,冯娜,等.航天员出舱充放电效应及防护技术研究［J/OL］.真空与低温，2020［2020-11-30］.http:∥kns.cnki.net/kcms/detail/62.1125.O4.20200918.0959.004.html．
TANG X, JI Q Z, FENG N, et al. A study of the charging and discharging effect to astronauts during extra vehicular activity and its elimination methods ［J/OL］. Vacuum and Cryogenics,2020［2020-11-30］. http:∥kns.cnki.net/kcms/detail/62.1125.O4.20200918.0959.004.html.(in Chinese)
［22］张悦，刘尚合，胡小锋，等．电晕放电辐射信号的探测系统与识别方法［J］．高电压技术，2014，40(9):2813-2819．
ZHANG Y, LIU S H, HU X F, et al. Detection system and identification method of electromagnetic signal radiated from corona discharge ［J］. High Voltage Engineering, 2014, 40(9): 2813-2819.(in Chinese)
［23］朱立颖，乔明，刘业楠，等．LEO航天器高压大功率太阳电池阵静电放电试验与分析［J］．航天器工程，2015,24(4):65-70．
ZHU L Y, QIAO M, LIU Y N, et al. Test and analysis on electrostatic discharge of high voltage and high power solar array for LEO spacecraft ［J］. Spacecraft Engineering, 2015,24(4): 65- 70.(in Chinese)
［24］冯娜,季启政,张絮洁,等.GEO卫星多层隔热组件充放电特性仿真［J/OL］.航空学报，2020［2020-11-30］.http:∥kns.cnki.net/kcms/detail/11.1929.V.20200915.1110.012.html.
FENG N, JI Q Z, ZHANG X J, et al. Simulation of charging and discharging characteristics of multi-layer thermal insulation
modules of GEO satellite ［J/OL］. Acta Aeronautica et Astronautica Sinica, 2020［2020-11-30］.http:∥kns.cnki.net/kcms/detail/11.1929.V.20200915.1110.012.html．(in Chinese)
［25］刘浩，刘尚合，魏明，等. 高空低气压电晕放电特性模拟试验研究［J］. 高电压技术， 2015，41(5)：1704-1708．
LIU H, LIU S H, WEI M, et al. Research of corona discharge characteristics for low pressure at high altitude based on simulation experiments［J］. High Voltage Engineering, 2015, 41(5): 1704-1708.(in Chinese)
［26］张百灵，王宇天，李益文，等. 低气压直流辉光放电数值模拟与实验研究［J］. 高电压技术，2016，42(3)：724-730．
ZHANG B L, WANG Y T, LI Y W, et al. Numerical simulation and experimental study for low-pressure direct-current glow discharge［J］. High Voltage Engineering, 2016, 42(3): 724-730.(in Chinese)
［27］段泽民，仇善良，司晓亮，等. 飞机静电放电器静电泄放性能的影响参数［J］. 高电压技术，2016，42(5)：1356-1362．
DUAN Z M, QIU S L, SI X L, et al. Parameters influencing the electrostatic discharge performance of aircraft static discharges［J］. High Voltage Engineering, 2016, 42(5): 1356-1362.（in Chinese）
［28］杨津基. 气体放电［M］. 北京：科学出版社，1983．
YANG J J. Gas discharge［M］. Beijing: Science Press, 1983.
［29］武占成，张希军，胡有志. 气体放电［M］. 北京：国防工业出版社，2012．
WU Z C, ZHANG X J, HU Y Z. Gas discharge［M］. Beijing: National Defense Industry Press, 2012.(in Chinese)
［30］胡孝勇. 气体放电及其等离子体［M］. 哈尔滨：哈尔滨工业大学出版社，1994．
HU X Y. Gas discharge and its plasma［M］. Harbin: Harbin Institute of Technology Press, 1994.(in Chinese)
［31］付洋洋. 低气压下气体放电相似性研究［M］. 北京：清华大学出版社，2018．
FU Y Y. Study on similarity of gas discharges at low pressure［M］. Beijing: Tsighua University Press, 2018.(in Chinese)

[1]	ZHENG Jiajia， KAN Junwu， HU Ming ， ZHANG Guang， WANG Jiong. Design of a Small-caliber Fuze Magnetorheological Grease Safety and Arming Device and Its Delay Time Characteristic [J]. Acta Armamentarii, 2019, 40(9): 1761-1769.
[2]	WANG Kai, WANG Jun-lin, XU Dong, GUO Tian-ji, WANG Wei, TU Jian. Research on Autocatalytic Thermal Decomposition Properties and Thermal Safety of NTO [J]. Acta Armamentarii, 2018, 39(9): 1727-1732.
[3]	XU Yong-hong, TONG Liang, SHI Zhi-cheng, ZHANG Hong-guang. Ignition Delay Characteristics of DME/H₂ Lean Mixtures at Low-to-medium Temperature [J]. Acta Armamentarii, 2018, 39(4): 655-663.
[4]	DENG Tong-ye, XU Qing-yao, SHEN Shuang-yan. Numerical Investigation on the Effect of NOx on Ignition Delay of Mathane [J]. Acta Armamentarii, 2017, 38(3): 476-482.
[5]	SHI Jian, LIU Zhong-le, WEN Wu-di. Study of the Magnetic Field Measurement of Electric Cable with Electrodes in Seawater [J]. Acta Armamentarii, 2015, 36(7): 1295-1301.
[6]	ZHANG Jia-wei, GONG Shen-guang, JIANG Run-xiang, CHEN Cong. Study of Electric Field Induced by Rotating Magnetic Dipole [J]. Acta Armamentarii, 2014, 35(2): 285-288.
[7]	LI Xian, WANG Qiu-liang, WANG Hou-sheng, LIU Jian-hua，CHEN Shun-zhong. Simulation and Experiment for Linear Induction Coil Propeller [J]. Acta Armamentarii, 2011, 32(11): 1389-1394.
[8]	LIU Wen-biao，CAO Yan-jie，ZHANG Yuan，ZOU Ben-gui. Structural Parameter Optimization of Synchronous Induction Coil Gun Based on Ant Colony Algorithm [J]. Acta Armamentarii, 2011, 32(11): 1416-1422.
[9]	DONG Gang, FAN Bao-chun, LI Hong-zhi. An Investigation on Instability of Deflagration and Detonation Induced by Conical Shock Wave [J]. Acta Armamentarii, 2010, 31(4): 401-408.
[10]	WU Zhi-liang， ZHANG He. The Magnetic Field Penetration Characteristics in Bore of Small Caliber Fuze Using Inductive Energy [J]. Acta Armamentarii, 2010, 31(10): 1310-1315.
[11]	SHANG Fu-jun, SHI Hong-gang, WANG You-qi,HUANG wei, TIAN Kai-wen, WU Hong. Researcn on the Preparation Technology of Nano Ta Powder Using Induction Plasma [J]. Acta Armamentarii, 2009, 30(8): 1119-1123.
[12]	MA Shao-jie, ZHANG He, LI Chang-sheng,SHI Lei. Simulation and Analysis of Fuze Link-belt Electromagnetic Induction Setting in Small Caliber Artillery [J]. Acta Armamentarii, 2009, 30(4): 419-424.
[13]	GU Ji-hui, SHI Xiang-quan, JANG Yang. Research on Improving Receiver Sensitivity of Electromagnetic Induction Devices in Adjacent Movement [J]. Acta Armamentarii, 2008, 29(5): 552-556.
[14]	CHEN Cong, ZHOU Jun, GONG Shen-guang. A New Method of Measuring the Alternating Electric Field of Ships in Lossy Medium [J]. Acta Armamentarii, 2006, 27(6): 998-1001.
[15]	Luo Ji, Tian Qingzheng, Jiang Haozheng. Analysis and Tests on the Non-LethaI Microwave Warhead [J]. Acta Armamentarii, 2001, 22(2): 173-177.