Study on an Impact Detection of Space Debris via Microwave
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- Soma Eriko
- 東京理科大学
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- Maki Kenichiro
- 理化学研究所
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- Takano Tadashi
- 宇宙航空研究開発機構宇宙科学研究本部
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- Sano Masatoshi
- 東京理科大学
Bibliographic Information
- Other Title
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- マイクロ波によるデブリ衝突検出系の検討
- マイクロハ ニ ヨル デブリ ショウトツ ケンシュツケイ ノ ケントウ
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Abstract
Microwave emissions due to hypervelocity impacts have been detected by heterodyne receivers in the ground experiments using an accelerator. We aim to establish the detection system of space debris impacts on a space structure via microwave. The emitted powers at several frequencies due to the impact velocity of 10km/sec are estimated from the characteristics at the experimental impact velocity. Considering the emitted power, the receiving antennas and the microwave frequencies, the maximum distances for detecting the microwave emission are 85m at 2GHz-band and 24m at 22GHz-band. The type and location of receiving antennas which can detect the impact on all habitation and experiment modules on the International Space Station are discussed. It is concluded that the impact can be sufficiently detected via a low gain antenna at 2GHz band.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 56 (650), 105-109, 2008
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
- 1390001204468605056
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- NII Article ID
- 10021152951
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 9419968
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed