Development of a Non-explosive Segmented Nut-type Holding and Release Mechanism for Cube Satellite Applications
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- OH Hyun-Ung
- Space Technology Synthesis Laboratory, Department of Aerospace Engineering, Chosun University
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- LEE Myoung-Jae
- Space Technology Synthesis Laboratory, Department of Aerospace Engineering, Chosun University
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抄録
A nylon cable cutting mechanism triggered by a nichrome burn wire is generally used for cube satellite applications for the purpose of holding and releasing onboard appendages owing to its simplicity and low cost. However, the disadvantages of this mechanism are a lower constraint force and also unavoidable system complexity when it is applied to cube satellites with multiple deployable structures. In this study, as the result of an internal development program for cube satellites, we propose a segmented nut-type holding and release mechanism that affords advantages such as high load capability and negligible induced shock. A demonstration model of the mechanism has been fabricated, assembled and functionally tested under qualification temperatures.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 58 (1), 1-6, 2015
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
- 1390001204080011392
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- NII論文ID
- 130004735474
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- NII書誌ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL書誌ID
- 026000768
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可