書誌事項
- タイトル別名
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- Development of a Boom for a 50kg-Class Micro-Satellite and Vibration Test
- 50kgキュウ コガタ エイセイ トウサイ ブーム ノ カイハツ ト シンドウ シケン
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The paper reports design process of a space boom to be installed in a 50kg-class micro-satellite, tentatively called as SOHLA-1. The total mass of the boom is 483g, while the length of the boom is 416mm. A spring-string type pin-puller was proposed. Vibration test with a bread-board model (BBM) of the boom leaded to an engineering model (EM) of the boom accommodated with a two-pin type pin-puller. Vibration test with the boom EM suggested some modifications to be made for a proto-type model (PM) of the boom. Vibration test, deployment test and thermal test on the boom PM confirmed feasibility of the flight model (FM) of the boom.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 55 (643), 406-410, 2007
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679446564224
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- NII論文ID
- 10020089885
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 8926567
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- 使用不可