積極的COTSを導入...

積極的COTSを導入した超小型推進系の開発とS-310-36号機による宇宙実証

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積極的COTSを導入した超小型推進系の開発とS-310-36号機による宇宙実証

Call No. (NDL)
Z74-B503
Bibliographic ID of National Diet Library
9318567
Material type
記事
Author
佐原 宏典ほか
Publisher
東京 : 日本航空宇宙学会
Publication date
2007-12
Material Format
Paper
Journal name
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 55(647) 2007.12
Publication Page
p.579~589
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Paper Digital

Material Type
記事
Author/Editor
佐原 宏典
中須賀 真一
Alternative Title
Development of propulsion system for microsatellite based on effective COTS, and its demonstration in S-310-36 sounding rocket experiment
Periodical title
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
No. or year of volume/issue
55(647) 2007.12
Volume
55
Issue
647
Pages
579~589