Advanced Search+
Liying ZHU (朱立颖), Zhigang LIU (刘治钢), Xiaofeng ZHANG (张晓峰), Chao WANG (王超), Xiaofei LI (李小飞), Bingxin ZHAO (赵冰欣). Study on volt-ampere characteristics of solar array arcs in LEO spacecraft[J]. Plasma Science and Technology, 2019, 21(2): 25302-025302. DOI: 10.1088/2058-6272/aaf18a
Citation: Liying ZHU (朱立颖), Zhigang LIU (刘治钢), Xiaofeng ZHANG (张晓峰), Chao WANG (王超), Xiaofei LI (李小飞), Bingxin ZHAO (赵冰欣). Study on volt-ampere characteristics of solar array arcs in LEO spacecraft[J]. Plasma Science and Technology, 2019, 21(2): 25302-025302. DOI: 10.1088/2058-6272/aaf18a

Study on volt-ampere characteristics of solar array arcs in LEO spacecraft

Funds: This work was supported by National Natural Science Foundation of China (No. 51407008).
More Information
  • Received Date: July 27, 2018
  • The primary and secondary arcs volt-ampere characteristics of low earth orbit solar arrays are studied in this research. Using three gallium-arsenide solar cell samples, the gap lengths of the solar cell are set to 1, 2, and 3 mm. First, the primary arc voltage characteristics of a solar array are analyzed. It is found that two steps are involved in the primary arc voltages, which are 116 and 22 V according to our experiment and are independent of the electrostatic discharge current and the gap lengths. By comparing with the arc pattern, we determined that current chopping may be the reason for the stepped arc voltage. Then, the characteristics of the secondary arc of the solar array are demonstrated. The study shows that the secondary arc voltage values increase with the gap length. In the case of the same cell with a fixed gap length, the voltage of the secondary arc increases with the string current. Finally, the relationship between the secondary arc voltage and the gap length is obtained which helps the string voltage and the gap length selection for system design.
  • [1]
    Ferguson D C 2007 Low Earth Orbit Spacecraft Charging Design Handbook (Washington, DC: NASA) NASA-HDBK-4006
    [2]
    Hastings D E, Weyl G and Kaufman D 1990 J. Spacecr. Rockets 27 539
    [3]
    Jongeward G A et al 2001 High voltage solar arrays for a direct drive hall effect propulsion system Proc. 27th Int.-Electric Propulsion Conf. (Pasadena, CA) (IEPC)
    [4]
    Hastings D and Garrett H 2004 Spacecraft-Environment Interactions (Cambridge: Cambridge University Press)
    [5]
    Ferguson D C, Snyder D B and Carruth R 1991 Findings of the Joint Workshop on Evaluation of Impacts of Space Station Freedom Ground Configurations (Washington, DC: NASA) NASA TM-103717 91N22370
    [6]
    Hosoda S et al 2006 IEEE Trans. Plasma Sci. 34 1986
    [7]
    Wright K H et al 2012 IEEE Trans. Plasma Sci. 40 334
    [8]
    Masui H et al 2012 IEEE Trans. Plasma Sci. 40 351
    [9]
    Cho M 2009 Electr. Eng. Japan 166 1
    [10]
    Galofaro J T, Vayner B and Hillard G B 2010 J. Spacecr. Rockets 47 521
    [11]
    Vayner B and Galofaro J T 2012 IEEE Trans. Plasma Sci. 40 388
    [12]
    Okumura T et al 2009 J. Spacecr. Rockets 46 689
    [13]
    Toyoda K et al 2012 IEEE Trans. Plasma Sci. 40 321
    [14]
    Lee T H and Greenwood A 1961 J. Appl. Phys. 32 916
    [15]
    Okumura T et al 2009 J. Spacecr. Rockets 46 697
    [16]
    Zhu L Y et al 2017 Plasma Sci. Technol. 19 055304
    [17]
    Masui H et al 2014 J. Spacecr. Rockets 51 922
  • Cited by

    Periodical cited type(3)

    1. Wei, D., Jianwen WU, J.W., Zhu, L. Study on plasma expansion model of primary discharge on spacecraft solar array. Plasma Science and Technology, 2024, 26(11): 115301. DOI:10.1088/2058-6272/ad718b
    2. Hongtao, R.. Analysis on Secondary arc Current of 500kV Power Station Transmission Line. 2020. DOI:10.1109/IFEEA51475.2020.00096
    3. Jiang, J., Zhao, M., Wen, Z. et al. Detection of DC series arc in more electric aircraft power system based on optical spectrometry. High Voltage, 2020, 5(1): 24-29. DOI:10.1049/hve.2019.0068

    Other cited types(0)

Catalog

    Article views (134) PDF downloads (266) Cited by(3)

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return