Department of Mechanical Engineering, Faculty of Engineering, Kobe University
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA)
Japan Ultra-high Temperature Materials Research Institute
Space Systems Department, IHI Aerospace
出版者
宇宙航空研究開発機構
出版者(英)
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料
雑誌名(英)
JAXA Special Publication: Proceedings of International Symposium on "SM/MPAC & SEED Experiment"
巻
JAXA-SP-08-015E
ページ
127 - 129
発行年
2009-03-31
会議概要(会議名, 開催地, 会期, 主催者等)(英)
International Symposium on "SM/MPAC & SEED Experiment" (International Congress Center EPOCHAL TSUKUBA, 10-11 March 2008)
抄録(英)
This paper describes upon the on orbit degradation of the MoS2 Bonded Film which are applied to external mechanism of Japanese Experiment Module (JEM) of International Space Station (ISS). The test articles were launched and kept on orbit for 1 year, 2 year and 3 year. Evaluation are performed by measuring adhesive property, friction property and surface properties of the MoS2 bonded film, HMB-34. Also ground environment exposure test were conducted to compare the degradation against on orbit exposed environment effect.
内容記述(英)
Physical characteristics: Original contains color illustrations