Study on a Reversible Thermal Panel for spacecraft (detailed design based on parametric studies and experimental verification)

Hosei Nagano, Akira Ohnishi, Yuji Nagasaka, Akira Nagashima

研究成果: Article査読

3 被引用数 (Scopus)

抄録

This paper describes a new passive thermal control device - a Reversible Thermal Panel (RTP), which changes its function reversibly from a radiator to solar absorber by deploying/stowing the radiator/absorber reversible fin. Parametric studies were conducted and the RTP configuration which satisfies the thermal requirements was determined. The RTP engineering model was fabricated using highly oriented graphite sheets, honeycomb base plate, and shape memory alloy. The heat rejection performances and autonomous thermal controllability were evaluated by thermal vacuum tests. The test results show the excellent performances of heat rejection, absorption, and autonomous thermal control for the RTP.

本文言語English
ページ(範囲)464-481
ページ数18
ジャーナルHeat Transfer - Asian Research
35
7
DOI
出版ステータスPublished - 2006 11月

ASJC Scopus subject areas

  • 凝縮系物理学
  • 流体および伝熱

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