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

doi:10.1002/htj.20131

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

Department of System Design Engineering

Research output: Contribution to journal › Article

2 Citations (Scopus)

Abstract

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.

Original language	English
Pages (from-to)	464-481
Number of pages	18
Journal	Heat Transfer - Asian Research
Volume	35
Issue number	7
DOIs	https://doi.org/10.1002/htj.20131
Publication status	Published - 2006 Nov 1

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Keywords

Deployable radiator
Graphite sheet
Light weight
Reversible thermal panel
Rotary actuator
Shape memory alloy
Solar absorber
Spacecraft thermal control

ASJC Scopus subject areas

Condensed Matter Physics
Fluid Flow and Transfer Processes

Cite this

Nagano, H., Ohnishi, A., Nagasaka, Y., & Nagashima, A. (2006). Study on a Reversible Thermal Panel for spacecraft (detailed design based on parametric studies and experimental verification). Heat Transfer - Asian Research, 35(7), 464-481. https://doi.org/10.1002/htj.20131

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Access to Document

10.1002/htj.20131