Discharges of plasma induced by hypervelocity impact on the solar array with different substrate structures1-Reference-Cited by-同舟云学术

Discharges of plasma induced by hypervelocity impact on the solar array with different substrate structures1

Published:2016-07-08 Issue:3 Volume:51 Page:337-347
ISSN:1383-5416
Container-title:International Journal of Applied Electromagnetics and Mechanics
language:
Short-container-title:JAE

Author:

Tang Enling¹,Li Zheng¹,Zhang Qingming²,Wang Meng¹,Xiang Shenghai¹,Liu Shuhua¹,He Liping¹,Han Yafei¹,Xia Jin¹,Wang Hongliang¹,Xu Mingyang¹

Affiliation:

1. School of Equipment Engineering, Shenyang Ligong University, Shenyang, Liaoning, China

2. State Key Laboratory of Explosive Science and Technique, Beijing Institute of Technology, Beijing, China

Publisher

IOS Press

Subject

Electrical and Electronic Engineering,Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,Electronic, Optical and Magnetic Materials

Reference15 articles.

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2. Fukushige S., Akahoshi Y., Watanabe K., Harano T., Machida Y., Furusawa N., Koura T., Hosoda S., Cho M. and Harada S., Hypervelocity impact test to solar array for evaluation of possibility of sustained arc. in Proc. 25th Int. Symp. Space Technol. Sci., 2006, 1356-1361.

3. Katz I., Mechanism for spacecraft charging initiated destruction of solar arrays in GEO. in Proc. AIAA 36th Aerosp. Sci. Meeting, Reno, NV, 1998, 98-1002.

4. Comparison of debris environment models. ORDEM2000, MASTER2001 and MASTER2005;Shinya;IHI Eng. Rev.,2007

5. Payan D., Schwander D. and Catani J.P., Risks of low-voltage arcs sustained by the photovoltaic power of a satellite solar array during an electrostatic discharge. Solar Array Dynamic Simulator, in Proc. 7th Spacecraft Charging Technol. Conf., 2001, 447.

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