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Charging Characteristics of Spacecraft Dielectric Material at Cryogenic Temperature

Research Project

Project/Area Number 26420816
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeMulti-year Fund
Section一般
Research Field Aerospace engineering
Research InstitutionTokyo City University

Principal Investigator

Watanabe Rikio  東京都市大学, 工学部, 准教授 (20308026)

Project Period (FY) 2014-04-01 – 2017-03-31
Project Status Completed (Fiscal Year 2016)
Budget Amount *help
¥5,070,000 (Direct Cost: ¥3,900,000、Indirect Cost: ¥1,170,000)
Fiscal Year 2016: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2015: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Fiscal Year 2014: ¥2,730,000 (Direct Cost: ¥2,100,000、Indirect Cost: ¥630,000)
Keywords体積抵抗率 / 極低温 / 宇宙機帯電 / 宇宙環境 / 静電放電 / 誘電体
Outline of Final Research Achievements

Charging analysis of spacecraft is necessary to prevent charging accident of spacecraft. In this study, volume resistivity of insulating material for spacecraft at cryogenic temperature was experimentally investigated because some spacecraft such as infrared space telescopes are operated at cryogenic temperature. The charge storage method was used to obtain volume resistivity from potential histories of dielectric films after electron irradiation. Experimental results of Kapton film indicated that the volume resistivity of short time region at 20 K increased by 569 times compared to room temperature. Surface potential remained kV order for several tens of days which may increase the risk of electrostatic discharge. The volume resistivity of the short time region showed the dependency according to exp(T-1/4).

Report

(4 results)
  • 2016 Annual Research Report   Final Research Report ( PDF )
  • 2015 Research-status Report
  • 2014 Research-status Report
  • Research Products

    (2 results)

All 2016 2014

All Presentation (2 results)

  • [Presentation] 宇宙機用誘電体材料の極低温下における帯電特性に関する研究2016

    • Author(s)
      澁谷優樹,渡邊力夫,宮坂明宏
    • Organizer
      第13回宇宙環境シンポジウム
    • Place of Presentation
      情報通信研究機構(東京)
    • Year and Date
      2016-11-01
    • Related Report
      2016 Annual Research Report
  • [Presentation] Surface Potential Characteristics of Electron Irradiated Coverglass for Spacecraft Solar Cell2014

    • Author(s)
      R. Watanabe, N. Higashiyama, K. Kawano, H. Miyake, M. Ohira, T. Okumura and M. Takahashi
    • Organizer
      13th Spacecraft Charging Technology Conference
    • Place of Presentation
      Pasadena, CA, USA
    • Year and Date
      2014-06-23 – 2014-06-27
    • Related Report
      2014 Research-status Report

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Published: 2014-04-04   Modified: 2018-03-22  

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