Preliminary results of rocket attitude and auroral green line emission rate in the DELTA campaign
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- Iwagami Naomoto
- Department of Earth and Planetary Science, University of Tokyo
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- Komada Sayaka
- Department of Earth and Planetary Science, University of Tokyo
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- Takahashi Takao
- Information Science Laboratory, Tokai University
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説明
The attitude of a sounding rocket launched in the DELTA (Dynamics and Energetics of the Lower Thermosphere in Aurora) campaign was determined with IR horizon sensors and geomagnetic sensors. Since the payload was separated into two portions, two sets of attitude sensors were needed. A new IR sensor was developed for the present experiment, and found the zenith-angle of the spin-axis of the rocket with an accuracy of 2°. By combining information obtained by both type of sensors, the absolute attitudes were determined. The auroral green line emission rate was measured by a photometer on board the same rocket launched under active auroral conditions, and the energy flux of the auroral particle precipitation was estimated.
収録刊行物
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- Earth, Planets and Space
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Earth, Planets and Space 58 (9), 1107-1111, 2006
地球電磁気・地球惑星圏学会 、公益社団法人 日本地震学会、特定非営利活動法人 日本火山学会、日本測地学会、日本惑星科学会
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詳細情報 詳細情報について
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- CRID
- 1390282681489399040
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- NII論文ID
- 10024493881
- 130003781230
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- NII書誌ID
- AA11211921
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- ISSN
- 18805981
- 13438832
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- NDL書誌ID
- 8084323
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
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