Development of Low Cost / Light Weight Oxidizer Tank in Hybrid Rocket
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- TATEYAMA Tetsuya
- 神奈川大学大学院工学研究科機械工学専攻 現 株式会社ジャムコ
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- TAKANO Atsushi
- 神奈川大学工学部機械工学科
Bibliographic Information
- Other Title
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- ハイブリッドロケットにおける低コスト・軽量酸化剤タンクの開発
Abstract
<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>
Journal
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- AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 19 (0), 19-26, 2020
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390283659849006720
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- NII Article ID
- 130007795269
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- ISSN
- 18840477
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed