Design Calculation of Heat Pipes and Heat Pipe Systems I. Sublimit Thermal Performance
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This lecture was mainly prepared by the second author, F.Polasek, during his stay in the Institute of Space and Astronautical Science as a visiting scientist for three months in 1988. The authors deeply appreciate this international promotion of science and technology by the Institute of Space and Astronautical Science. Also financial support for him from Japan Association for Heat Pipes is acknowledged with appreciation.
資料番号: SA0033632000
収録刊行物
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- The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1988
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The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1988 9 87-134, 1989-03
宇宙科学研究所
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詳細情報 詳細情報について
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- CRID
- 1050848249891069952
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- NII論文ID
- 110000028428
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- NII書誌ID
- AA10455137
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- ISSN
- 0288433X
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- Web Site
- http://id.nii.ac.jp/1696/00031345/
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- 本文言語コード
- en
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- 資料種別
- departmental bulletin paper
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- データソース種別
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- IRDB
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