書誌事項
- タイトル別名
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- Research on Direct Filament Winding Multi-Segment Rocket Motor
説明
Breakthrough technologies are needed to enhance the ability of rocket motor. In this research, the manufacturing method of conventional rocket motors has been dramatically changed by using the Multi-Segment Technology and Direct Filament Winding (DFW) Technology. These technologies enable a great increase of propellant mass ratio, Multi-Thrust and improvement in flight performance. A triple thrust pattern and 2-pulse thrust were demonstrated by static firing tests of prototype rocket motors manufactured using the Multi-Segment Technology and DFW technology. From a flight performance analysis, flight range extension by 60% and terminal velocity enhancement by 50% can be expected when these technologies are applied to a φ0.3m-class rocket.
収録刊行物
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- スペース・エンジニアリング・コンファレンス講演論文集
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スペース・エンジニアリング・コンファレンス講演論文集 2017.26 (0), 1B1-, 2017
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
- 1390001288039040640
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- NII論文ID
- 130007411212
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- ISSN
- 24243191
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可