太阳电池阵静电放电脉冲电流及其辐射信号特性的研究
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- 英文论文题名：Current and Characteristics of Electrostatic Discharge Signal on the Solar Array
- 论文作者：李存惠 ; 柳青 ; 杨生胜 ; 苗育君 ; 郑阔海 ; 秦晓刚
- 英文论文作者：LI Cunhui ; LIU Qing ; YANG Shengsheng ; MIAO Yujun ; ZHENG Kuohai ; QIN Xiaogang
- 年：2015
- 作者机构：兰州空间技术物理研究所真空技术与物理重点实验室;
- 论文关键词：太阳电池阵 ; 静电放电 ; 放电电流 ; 时域 ; 频域 ; 辐射场
- 英文论文关键词：solar array ; electrostatic discharge ; discharge current ; time-domain ; frequency-domain ; radiation field
- 会议召开时间：2015-08-12
- 会议录名称：静电放电：从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议论文集
- 语种：中文
- 分类号：V442
- 学会代码：WLJD
- 会议名称：静电放电 ; 从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议
- 会议地点：中国河北石家庄
- 主办单位：中国物理学会静电专业委员会
- 学会名称：中国物理学会静电专业委员会
- 页数：4
- 文件大小：634k
- 原文格式：D
- 会议级别：全国
摘要
研究太阳电池阵静电放电的时域和频域特征,为掌握太阳电池阵充放电形成机制提供依据。静电放电地面模拟试验在SCF-900航天器带电地面综合模拟试验装置中完成,通过电子辐照方法进行太阳电池阵静电放电试验。试验中将太阳电池阵结构与真空室地隔离,利用电子枪模拟GEO轨道最坏空间带电环境,通过电子枪辐照样品表面使其充电,当积累电子产生的负电位超过太阳电池材料的电压击穿阈值时,在电池阵表面会发生静电放电。利用电流探头CT-2(1mV/1mA)、单极子天线和数字存储示波器Terk DPO4104(带宽1GHz,采样频率5GHz)来测量电流、电场并记录其波形。太阳电池阵表面充电静电电位是产生静电放电的放电源,放电过程中激发出脉冲宽度为几μs的瞬态放电电流,产生的脉冲电流峰-峰值幅度为几安培到十几安培,波形是幅度逐渐衰减的振铃波。太阳电池阵静电放电辐射场持续时间几百ns至几个μs的瞬态信号,辐射场强度为几千V/m,其频谱覆盖了零到几百MHz的范围。太阳电池阵静电放电太阳电池阵静电放电的时域特征表现为脉冲群,信号波形具有陡峭的前沿,频率范围主要集中在0~50MHz之间。该结论对于实测航天器静电放电信号特征具有重要的参考价值。
To study the characteristics of time and frequency domain of solar arrays during electrostatic discharge,to improve the understanding as well as technical support on charge-discharge mechanism of solar arrays.Electrostatic discharge ground simulation was conducted in an electrified synthesis facility of SCF-900 by a test of electron irradiation on solar arrays.In the test,the main structure of solar arrays was isolated from the ground of vacuum chamber and electron gun was used to simulate the electrified environmental extremes in the geostationary earth orbit.Specimens was electronically irradiated and charged by the electron gun.Electrostatic discharge was observed on the solar array surface once the negative potential of solar array caused by accumulated electrons exceeded its voltage breakdown threshold.Devices were used to record the current strength and shape as well as the electrical field,including the monopoles,the CT-2 current detectors(1mv/m A)and the Terk DPO4104 digital storage oscilloscope(bandwidth 1GHz and sampling frequency 5GHz).Electrostatic discharge was initiated by the electrostatic potential of surface charged solar arrays.A transient current was activated during the discharge and its pulse width is 10~(-6)s.A degraded ring-wave current was observed and the detected pulse peak ranged from several to dozen amperes.The solar arrays electrostatic discharge field sustains from 10~(-7) to 10~(-6)s.The irradiation field strength was 10~3V/m and the spectrum ranged up to 10~2MHz.A pulse cluster was characterized for the solar arrays time domain,showing a steep-front,the frequency ranged from 0-50MHz.Such results is valuable for the physical testing on the spacecraft electrostatic discharge signals.
To study the characteristics of time and frequency domain of solar arrays during electrostatic discharge,to improve the understanding as well as technical support on charge-discharge mechanism of solar arrays.Electrostatic discharge ground simulation was conducted in an electrified synthesis facility of SCF-900 by a test of electron irradiation on solar arrays.In the test,the main structure of solar arrays was isolated from the ground of vacuum chamber and electron gun was used to simulate the electrified environmental extremes in the geostationary earth orbit.Specimens was electronically irradiated and charged by the electron gun.Electrostatic discharge was observed on the solar array surface once the negative potential of solar array caused by accumulated electrons exceeded its voltage breakdown threshold.Devices were used to record the current strength and shape as well as the electrical field,including the monopoles,the CT-2 current detectors(1mv/m A)and the Terk DPO4104 digital storage oscilloscope(bandwidth 1GHz and sampling frequency 5GHz).Electrostatic discharge was initiated by the electrostatic potential of surface charged solar arrays.A transient current was activated during the discharge and its pulse width is 10~(-6)s.A degraded ring-wave current was observed and the detected pulse peak ranged from several to dozen amperes.The solar arrays electrostatic discharge field sustains from 10~(-7) to 10~(-6)s.The irradiation field strength was 10~3V/m and the spectrum ranged up to 10~2MHz.A pulse cluster was characterized for the solar arrays time domain,showing a steep-front,the frequency ranged from 0-50MHz.Such results is valuable for the physical testing on the spacecraft electrostatic discharge signals.
引文
[1]Miyake H,Honjoh M,Maruta Y,et al.Space charge accumulation in polymeric materials for spacecraft irradiated electron and proton[C].Annual Report Conference on Electrical Insulation and Dielectric Phenomena,CEIDP,2007.
[2]Piacentini R,Ripoli C,Mezzogori D,et al.Experimental Investigation and Method of Mathematical Modeling of Electrostatic Discharges[J].Journal of Spacecraft and Rockets,2011,48(2):266-270.
[3]Yadlowsky,E.J;Churchill,R.J;Hazelton,R.C.Laboratory simulation of irradiation-induced dielectric breakdown in spacecraft charging[R].NASA-CR-162762 80N17135,Feb 13,1980.
[4]李凯,王立,秦晓刚,等.地球同步轨道高压太阳电池阵充放电效应研究[J].航天器环境工程,2008,25(2):125-128.
[5]薛梅.高压砷化镓太阳阵ESD效应及防护技术研究[D].天津,中国:天津大学,2007.
[6]李凯,李得天,秦晓刚,等.空间太阳阵表面静电放电特性实验研究[J].真空科学与技术学报,2013,33(10):1007-1010.
[7]Yuan Qingyun;Sun yongwei;Cao Hefei.Electrostatic Discharge Effects on the High-voltage Solar Array[J].Journal of Higll Voltage Engineering,2013,39(10):2392-2397.
[8]Adamo R,Nanevicz J,Hilbers G.Development of the Transient Pulse Monitor(TPM)for SCATHA/P78-2[C].Proceedings of the Spacecraft Charging Technology Conference,1978.
[9]Wilson P,Ma M.Fields Radiated by Electrostatic Discharges[J].IEEE Transactions on Electromagnetic Compatibility,1991,33(1):10~18.
[10]杜磊,刘卫东,王阳阳.静电放电小空间测试装置性能分析与验证实验[J].高电压技术,2012,38(9):2248-2253.
[11]宋文武,张传东,刘义,等.基于光纤信号传输的核电磁脉冲场探测仪的设计与实现[J].核电子学与探测技术,2007,27(2):246-249.
[12]原青云,刘尚合,张希军,等.电晕电流及其辐射信号特性的研究[J].高电压技术,2008,34(8):1547-1551.
[13]周星,魏光辉,张希军.ESD辐射场的计算及对传输线的耦合研究[J].高电压技术,2008,34(4):670-673.
[14]Wang P,Zhang Guixin.The Measurement Method for Corona Discharge Current Under High-Voltage Environment[J].IEEE Transactions on Instrumentation and Measurement,2008.57(8):1786~1790.
[15]Jenngho K,Takashi K,Yoshio S,et al.Solar Array ESD Ground Tests in Simulated GEO Environment[C].43rd AIAA Aerospace Sciences Meeting and Exhibit.Reno,Nevada:AIAA,2005:1-8.
[16]Chn M,Ramasamy R,Maswanoto T,et al.Laboratory tests on 110-Volt solar arrays in simulated geosynehronons orbit environment[J].Journal of Spacecraft and Rockets,2003,40(2):211-220.
[17]Chubb J.Measurement of charge transfer in electrostatic discharges[J].Journal of Electrostatics,2006,64(2):302-305.
[18]吴健静电放电(ESD)辐射特性的研究[D].哈尔滨,中国:哈尔滨工业大学,2009.
[19]Honda,M.Indirect ESD measurement using a short monopole antenna[C].IEEE International Symposium on Electromagnetic Compatibility Symposium Record,1990:641-645.
[20]Honda,M.Impulsive fields generated by low-voltage ESD[C].IEEE Industry Applications Society Annual Meeting,1991,1:577-580.
[21]Honda,M.A new threat-EMI effect by indirect ESD on electronic equipment[J].IEEE Transactions on Industry Applications,1994,25(5):939-944.
[22]Danabalan TL,Ghatpande ND,Shastry SVK,et al.Antenna for Transient Pulse Monitor Subsystem[C].Proceedings of the 9th International Conference on Electro Magnetic Interference and Compatibility,INCEMIC,2006.
[23]Frezet M,Granger J P,Levy L,et al.Assessment of charging behavior of meteosat in geosynchronous environment[J].IEEE Transactions on Nuclear Science,1998,35(6):1400-1406.
[24]Mulholland J,Dunn T.The measurement of solar array discharges in a simulated space environment[J].IEEE Transactions on Electromagnetic Compatibility,1994,36(2):97-103.
[2]Piacentini R,Ripoli C,Mezzogori D,et al.Experimental Investigation and Method of Mathematical Modeling of Electrostatic Discharges[J].Journal of Spacecraft and Rockets,2011,48(2):266-270.
[3]Yadlowsky,E.J;Churchill,R.J;Hazelton,R.C.Laboratory simulation of irradiation-induced dielectric breakdown in spacecraft charging[R].NASA-CR-162762 80N17135,Feb 13,1980.
[4]李凯,王立,秦晓刚,等.地球同步轨道高压太阳电池阵充放电效应研究[J].航天器环境工程,2008,25(2):125-128.
[5]薛梅.高压砷化镓太阳阵ESD效应及防护技术研究[D].天津,中国:天津大学,2007.
[6]李凯,李得天,秦晓刚,等.空间太阳阵表面静电放电特性实验研究[J].真空科学与技术学报,2013,33(10):1007-1010.
[7]Yuan Qingyun;Sun yongwei;Cao Hefei.Electrostatic Discharge Effects on the High-voltage Solar Array[J].Journal of Higll Voltage Engineering,2013,39(10):2392-2397.
[8]Adamo R,Nanevicz J,Hilbers G.Development of the Transient Pulse Monitor(TPM)for SCATHA/P78-2[C].Proceedings of the Spacecraft Charging Technology Conference,1978.
[9]Wilson P,Ma M.Fields Radiated by Electrostatic Discharges[J].IEEE Transactions on Electromagnetic Compatibility,1991,33(1):10~18.
[10]杜磊,刘卫东,王阳阳.静电放电小空间测试装置性能分析与验证实验[J].高电压技术,2012,38(9):2248-2253.
[11]宋文武,张传东,刘义,等.基于光纤信号传输的核电磁脉冲场探测仪的设计与实现[J].核电子学与探测技术,2007,27(2):246-249.
[12]原青云,刘尚合,张希军,等.电晕电流及其辐射信号特性的研究[J].高电压技术,2008,34(8):1547-1551.
[13]周星,魏光辉,张希军.ESD辐射场的计算及对传输线的耦合研究[J].高电压技术,2008,34(4):670-673.
[14]Wang P,Zhang Guixin.The Measurement Method for Corona Discharge Current Under High-Voltage Environment[J].IEEE Transactions on Instrumentation and Measurement,2008.57(8):1786~1790.
[15]Jenngho K,Takashi K,Yoshio S,et al.Solar Array ESD Ground Tests in Simulated GEO Environment[C].43rd AIAA Aerospace Sciences Meeting and Exhibit.Reno,Nevada:AIAA,2005:1-8.
[16]Chn M,Ramasamy R,Maswanoto T,et al.Laboratory tests on 110-Volt solar arrays in simulated geosynehronons orbit environment[J].Journal of Spacecraft and Rockets,2003,40(2):211-220.
[17]Chubb J.Measurement of charge transfer in electrostatic discharges[J].Journal of Electrostatics,2006,64(2):302-305.
[18]吴健静电放电(ESD)辐射特性的研究[D].哈尔滨,中国:哈尔滨工业大学,2009.
[19]Honda,M.Indirect ESD measurement using a short monopole antenna[C].IEEE International Symposium on Electromagnetic Compatibility Symposium Record,1990:641-645.
[20]Honda,M.Impulsive fields generated by low-voltage ESD[C].IEEE Industry Applications Society Annual Meeting,1991,1:577-580.
[21]Honda,M.A new threat-EMI effect by indirect ESD on electronic equipment[J].IEEE Transactions on Industry Applications,1994,25(5):939-944.
[22]Danabalan TL,Ghatpande ND,Shastry SVK,et al.Antenna for Transient Pulse Monitor Subsystem[C].Proceedings of the 9th International Conference on Electro Magnetic Interference and Compatibility,INCEMIC,2006.
[23]Frezet M,Granger J P,Levy L,et al.Assessment of charging behavior of meteosat in geosynchronous environment[J].IEEE Transactions on Nuclear Science,1998,35(6):1400-1406.
[24]Mulholland J,Dunn T.The measurement of solar array discharges in a simulated space environment[J].IEEE Transactions on Electromagnetic Compatibility,1994,36(2):97-103.