Thermal Control System for Space Experiment on Two-Phase Boiling Flow -I ; Analysis and Design of Condenser

Ryoji IMAI; Koichi SUZUKI; Haruo KAWASAKI; Chungpyo HONG; Hiroya ISHIZUKA; Kiyosumi FUJII; Yasuhisa SHINMOTO; Haruhiko OHTA

doi:10.15011/jasma.28.2.109

Ryoji IMAI , Koichi SUZUKI, Haruo KAWASAKI, Chungpyo HONG, Hiroya ISHIZUKA, Kiyosumi FUJII, Yasuhisa SHINMOTO, Haruhiko OHTA

著者情報

Ryoji IMAI [日本] 責任著者
Heat & Fluid Dynamics Dept., Research Laboratory IHI Corporation [日本]
Koichi SUZUKI [日本]
Dept. Mechanical Eng., Tokyo University of Science [日本]
Haruo KAWASAKI [日本]
Thermal Systems Group Aerospace Research and Development Directorate (ARD), Japan Aerospace Exploration Agency(JAXA) [日本]
Chungpyo HONG [日本]
Dept. Mechanical Eng., Tokyo University of Science [日本]
Hiroya ISHIZUKA [日本]
Institute of Space and Astronatical Science ISS Science Project Office Japan Aerospace Exploration Agency [日本]
Kiyosumi FUJII [日本]
Institute of Space and Astronatical Science ISS Science Project Office Japan Aerospace Exploration Agency [日本]
Yasuhisa SHINMOTO [日本]
Faculty of Engineering Department of Aeronautics and Astronautics Kyushu University [日本]
Haruhiko OHTA [日本]
Faculty of Engineering Department of Aeronautics and Astronautics Kyushu University [日本]

ジャーナルオープンアクセス

2011 年 28 巻 2 号 p. 109-

DOI https://doi.org/10.15011/jasma.28.2.109

詳細

抄録

Design of condenser planned to be installed on boiling flow experiment on ISS was conducted. In this condenser, rectangular vapor tube was installed on flat type cold plate which had experienced on-orbit experiments. Arithmetic thermal model was constructed, which considered tube wall conductivity, heat transfer coefficient on condensation and cooling water flow. Specification of condenser which can condensate vapor of 400W was determined through analysis by this arithmetic model.

責任著者(Corresponding author)

J-STAGEへの登録はこちら（無料）