Development of Transient Mathematical Model of Loop Heat Pipe and Verification in Orbit
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- NAGANO Hosei
- Corresponding author
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- AKIZUKI Yuki
- 宇宙航空研究開発機構 研究開発部門
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- OKAMOTO Atsushi
- 宇宙航空研究開発機構 研究開発部門
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- SATO Koki
- 宇宙航空研究開発機構 研究開発部門
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- MIYAKITA Takeshi
- 宇宙航空研究開発機構 研究開発部門
Bibliographic Information
- Other Title
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- ループヒートパイプ過渡熱流動モデルの開発と宇宙軌道上での検証
- ループヒートパイプ カト ネツ リュウドウ モデル ノ カイハツ ト ウチュウ キドウ ジョウ デ ノ ケンショウ
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Description
<p>This paper discusses the transient model of loop heat pipes in detail. A new model was constructed using an implicit method for fluid calculations and an explicit method for heat transfer calculations between pipe walls and radiators. In addition, the effectiveness of this model was verified using a loop heat pipe used for demonstration purposes on International Space Station. Good agreement was shown with the results of thermal vacuum tests. On the other hand, a comparison with the on-orbit test results revealed differences in vibration phenomena. It was concluded that this was because the heat input in orbit, such as solar heat input, was not accurately estimated.</p>
Journal
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- JAPANESE JOURNAL OF MULTIPHASE FLOW
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JAPANESE JOURNAL OF MULTIPHASE FLOW 38 (1), 15-23, 2024-03-15
THE JAPANESE SOCIETY FOR MULTIPHASE FLOW
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Details 詳細情報について
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- CRID
- 1390581401102949376
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- NII Book ID
- AN10088286
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- ISSN
- 18815790
- 09142843
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- NDL BIB ID
- 033415016
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL Search
- Crossref
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- Abstract License Flag
- Disallowed