J4 ›› 2013, Vol. 51 ›› Issue (01): 116-119.
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ZHOU Qing1, WANG De jun2, ZHAO Guang yi1, MA Yu gang1, ZHAO Bao kui1, YI Hai yun1, WANG Zhen chao1, NIU Lu ying1
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Abstract:
Aiming at the operating faults of geosynchronous orbit satellite due to medium’s internal charging, we put forward Monte Carlo method to simulate the process of the medium’s internal charging. The plate model charging process of spacecraft medium is simplified as electron crossing the screen of aluminium into epoxy. With the help of the MCNP software, we obtained the results that different thicknesses of aluminium and different electron energies influence on the largest electric field of medium.
Key words: internal charging, MCNP software, electron
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ZHOU Qiang, WANG De-Jun, DIAO An-Xi, MA Yu-Gang, DIAO Bao-Kui, YI Hai-Yun, WANG Zhen-Chao, NIU Lu-Ying. MCNP Simulate the Internal Dielectric Charging Process of Satellites[J].J4, 2013, 51(01): 116-119.
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http://xuebao.jlu.edu.cn/lxb/EN/Y2013/V51/I01/116
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