書誌事項
- タイトル別名
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- Development of Low Cost / Light Weight Oxidizer Tank in Hybrid Rocket
抄録
<p>To inexpensive and quickly launch microsatellites, ultra-small hybrid rockets have been developed. The current goal to us is to reach an altitude of 100 km in 2020. In order to develop a rocket that reaches a higher altitude in the future, it is necessary to develop the oxidizer tank to be lightweight, large-sized, and low-cost. For this reason, we started in house developed oxidizer tanks from fiscal 2017 and recorded the highest altitude of 4.8 km in the same year. This research reported the results of the 2018 oxidizer tank development.</p>
収録刊行物
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- 航空宇宙技術
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航空宇宙技術 19 (0), 19-26, 2020
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
- 1390283659849006720
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- NII論文ID
- 130007795269
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- ISSN
- 18840477
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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