書誌事項
- タイトル別名
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- 1026 Development of Launcher to Simulate Debris Impacts in GEO
抄録
In order to simulate the debris impacts in geosynchronous orbit, we need the launcher that can launch the projectile under approximately 1[km/sec]. We converted a two-stage light gas gun into a powder gun. In generally, though sabot separation technique is used to launch the projectile of sphere, we can not apply its technique to a our powder gun. So we also conducted the development of new separation technique of projectile of sphere. In particular, we will show with the focus on the new separation technique.
収録刊行物
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- 年次大会講演論文集
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年次大会講演論文集 2006.5 (0), 345-346, 2006
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
- 1390001206062330880
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- NII論文ID
- 110006635572
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- ISSN
- 24331325
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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