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- IZUTSU Naoki
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- AKITA Daisuke
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- FUKE Hideyuki
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- IIJIMA Issei
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- KATO Yoichi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- KAWADA Jiro
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- MATSUSHIMA Kiyoho
- Fujikura Parachute Company
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- MATSUZAKA Yukihiko
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- MIZUTA Eiichi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- NAKADA Takashi
- Fujikura Parachute Company
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- NONAKA Naoki
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- SAITO Yoshitaka
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- TAKADA Atsushi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- TAMURA Keisuke
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- YAMADA Kazuhiko
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- YOSHIDA Tetsuya
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Abstract
A zero-pressure balloon used for scientific observation in the stratosphere has an unmanageable limitation that its floating altitude decreases during a nighttime because of temperature drop of the lifting gas. Since a super-pressure balloon may not change its volume, the lifetime can extend very long. We had introduced so called the ‘lobed-pumpkin’ type of super-pressure balloon that can realize a full-scale long-duration balloon and it will be in practical use in the very near future. As for larger super-pressure balloons, however, we still have some potential difficulties to be resolved. We here propose a new design suitable for a larger super-pressure balloon, which is roughly ‘lobed pumpkin with lobed cylinder’ and can adapt a single design for balloons of a wide range of volumes. Indoor inflation tests were successfully carried out with balloons designed and made by the method. It has been shown that the limit of the resisting pressure differential for a new designed balloon is same as that of a normal lobed-pumpkin balloon.
Journal
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 8 (ists27), Pm_7-Pm_13, 2010
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282680297301248
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- NII Article ID
- 130000450585
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- ISSN
- 18840485
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- Text Lang
- en
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed