Proposal of Microgravity Experiments on Forced Convection Boiling in Orbit

被引：0

作者：

Ohta, Haruhiko ^{[1
]}

Asano, Hitoshi ^{[2
]}

Kawanami, Osamu ^{[3
]}

Imai, Ryoji ^{[4
]}

Suzuki, Koichi ^{[5
]}

Shinmoto, Yasuhisa ^{[1
]}

Abe, Yoshiyuki ^{[6
]}

Tanaka, Koutaro ^{[7
]}

Savino, Raffaele ^{[8
]}

Yoda, Shinichi

Matsumoto, Satoshi ^{[9
]}

Fujii, Kiyosumi ^{[9
]}

Kawasaki, Haruo ^{[9
]}

Ishizuka, Hiroya ^{[9
]}

Okamoto, Atsushi ^{[9
]}

Murakami, Keiji ^{[9
]}

Uchida, Takashi ^{[9
]}

Kobayashi, Toshikazu ^{[9
]}

Kobayashi, Ryoji ^{[9
]}

Ohkubo, Kengoh ^{[9
]}

Shinozaki, Shinichi ^{[10
]}

Kogure, Kazumi ^{[10
,11
]}

Murakami, Atsuhi ^{[11
]}

Ueda, Yukihiro ^{[11
]}

Nakagawa, Yoko ^{[11
]}

机构：

[1] Kyushu Univ, Nishi Ku, 744 Motooka, Fukuoka 8190395, Japan

[2] Kobe Univ, Nada Ku, Kobe, Hyogo 6578501, Japan

[3] Univ Hyogo, Kobe, Hyogo 6712201, Japan

[4] IHI Corp, Isogo Ku, Yokohama, Kanagawa 2358501, Japan

[5] Tokyo Univ Sci, Noda, Chiba 2788510, Japan

[6] AIST, Tsukuba, Ibaraki 3058568, Japan

[7] Shibaura Inst Technol, Koto Ku, Tokyo 1358548, Japan

[8] Univ Naples Federico II, I-80014 Naples, Italy

[9] Japan Aerosp Explorat Agcy, Tsukuba, Ibaraki 3058505, Japan

[10] Japan Space Forum, Chiyoda Ku, Tokyo 1000004, Japan

[11] IHI Aerosp Co Ltd, Gunma 3702398, Japan

来源：

INTERNATIONAL JOURNAL OF MICROGRAVITY SCIENCE AND APPLICATION | 2009年 / 26卷 / 03期

关键词：

flow boiling; two-boiling; microgravity; reduced gravity; ISS;

D O I：

暂无

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

Increase in the satellite size and corresponding power consumption requires the development of thermal management system handling a large amount of waste heat and its transportation along a long distance to the radiators. Boiling and two-phase flow becomes a powerful means for this purpose because it transports latent heat of vaporization. It minimizes the size of cold plates, liquid flow rate, i.e. pump power, and launch mass. In the present paper, ISS experiment on forced convection boiling is proposed to obtain the data for the design of the high performance space thermal management systems based on the analysis of liquid-vapor flow structures and heat transfer characteristics under microgravity conditions. Subjects to be investigated in the proposed experiment and the outline of experimental setup are clarified.

引用

页码：213 / 217

页数：5

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