710 宇宙用マスドライバ : プロトタイプモデルの性能評価(領域7 ダイナミクスと制御)
書誌事項
- タイトル別名
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- 710 Evaluation experiment of Prototype Model of a Mass Driver for Space Crafts
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説明
In recent years, a concept has been proposed that microsatellites be equipped with a mass driver, which exerts kinetic energy on a solid object accelerate and eject it into space using such means of acceleration as compressed gases, explosives, and electromagnetic force. Mass drivers will enable more missions and allow the realization a number of conceptualized ideas including the creation of artificial shooting star generators and the attitude control of troubled satellites in space debris measurement. This report focuses on a mass driver that is powered by compressed gas and designed to be mounted on a microsatellite; the basic performances and characteristics are evaluated with an on-ground experimental prototype model. Experiments and evaluations cover the following: ejection capability, including variations in ejection speed; effect of the tubing length, which ensures the flexibility of satellite design; and durability in vibration during the launch. Results of the various experiments confirm that the prototype model has a sufficient level of acceleration performance and vibration durability for use in spacecraft.
収録刊行物
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- 機械力学・計測制御講演論文集
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機械力学・計測制御講演論文集 2014 "710-1"-"710-8", 2014-08-25
一般社団法人日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1573105977709984768
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- NII論文ID
- 110009982579
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- NII書誌ID
- AA11901770
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- ISSN
- 13480235
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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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- CiNii Articles