書誌事項
- タイトル別名
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- A New Variable-Emittance Radiator Equipped on a Spacecraft “HAYABUSA”
- 「 ワ ヤブサ 」 ニ トウサイ サレタ シンキ ナ ネツ ホウシャリツ カヘン ソシ
- A New Variable-Emittance Radiator Equipped on a Spacecraft ^|^ldquo;HAYABUSA^|^rdquo;
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説明
Thermal control is one of the most important issues in designing a spacecraft. A light, reliable, and inexpensive thermal-control device is strongly demanded. We have developed a new thermal-control device, Smart Radiation Device (SRD), based on a metal-insulator transition of (La, Sr) MnO3 perovskite-structure oxides. The emittance property of the device changes significantly at the transition temperature near room temperature; high at high temperatures whereas low at low temperatures. Thus, the device automatically controls the emmisive heat transfer from the spacecraft without the need for any mechanical parts and electrical power. The practical validity of the device was demonstrated in the recent flight of a spacecraft “HAYABUSA”. The developed oxide-thin-film radiator also greatly reduces the weight and production cost of the thermal control devices.
収録刊行物
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- 表面科学
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表面科学 33 (12), 675-680, 2012
公益社団法人 日本表面科学会
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詳細情報 詳細情報について
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- CRID
- 1390001206457012352
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- NII論文ID
- 130004486724
- 10031136974
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- NII書誌ID
- AN00334149
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- COI
- 1:CAS:528:DC%2BC3sXksFKksrc%3D
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- ISSN
- 18814743
- 03885321
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- NDL書誌ID
- 024154432
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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
- NDL
- Crossref
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- 抄録ライセンスフラグ
- 使用不可