Heat rejection/retention characteristics of a re-deployable radiator for venus exploration mission

Hosei Nagano; Akira Ohnishi; Ken Higuchi; Kan Matsumoto; Yu Oikawa; Kazuki Watanabe; Yuji Nagasaka

doi:10.4271/2007-01-3241

Heat rejection/retention characteristics of a re-deployable radiator for venus exploration mission

Hosei Nagano, Akira Ohnishi, Ken Higuchi, Kan Matsumoto, Yu Oikawa, Kazuki Watanabe, Yuji Nagasaka

システムデザイン工学科

研究成果: Conference article › 査読

抄録

This paper experimentally and analytically evaluates the heat rejection/retention performance of a reversible thermal panel (RTP) which can autonomously change thermal performance depending on its own thermal conditions. The RTP is considered as a candidate methodology for thermal control of Venus mission, PLANET-C, in order to save survival heater power. An RTP prototype was tested and evaluated. An analytical thermal model of the RTP was also developed, and basic performances of the RTP were evaluated. Thermal performance of the RTP when applied to the longwave camera (LIR) of the PLANET-C was evaluated with an analytical thermal model as functions of fin deployment directions and rear surface properties of the RTP's fin. The analytical results showed that the RTP can save heater power in comparison to a conventional radiator.

本文言語	English
ジャーナル	SAE Technical Papers
DOI	https://doi.org/10.4271/2007-01-3241
出版ステータス	Published - 2007 1 1
イベント	37th International Conference on Environmental Systems, ICES 2007 - Chicago, IL, United States 継続期間: 2007 7 9 → 2007 7 12

ASJC Scopus subject areas

Automotive Engineering
Safety, Risk, Reliability and Quality
Pollution
Industrial and Manufacturing Engineering

文献へのアクセス

10.4271/2007-01-3241

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引用スタイル

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abstract = "This paper experimentally and analytically evaluates the heat rejection/retention performance of a reversible thermal panel (RTP) which can autonomously change thermal performance depending on its own thermal conditions. The RTP is considered as a candidate methodology for thermal control of Venus mission, PLANET-C, in order to save survival heater power. An RTP prototype was tested and evaluated. An analytical thermal model of the RTP was also developed, and basic performances of the RTP were evaluated. Thermal performance of the RTP when applied to the longwave camera (LIR) of the PLANET-C was evaluated with an analytical thermal model as functions of fin deployment directions and rear surface properties of the RTP's fin. The analytical results showed that the RTP can save heater power in comparison to a conventional radiator.",

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T1 - Heat rejection/retention characteristics of a re-deployable radiator for venus exploration mission

AU - Nagano, Hosei

AU - Ohnishi, Akira

AU - Higuchi, Ken

AU - Matsumoto, Kan

AU - Oikawa, Yu

AU - Watanabe, Kazuki

AU - Nagasaka, Yuji

PY - 2007/1/1

Y1 - 2007/1/1

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