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

Research output: Contribution to journalArticle

1 Citation (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 languageEnglish
Pages (from-to)464-481
Number of pages18
JournalHeat Transfer - Asian Research
Volume35
Issue number7
DOIs
Publication statusPublished - 2006 Nov

Fingerprint

spacecraft design
Spacecraft
radiators
rejection
absorbers
thermal vacuum tests
heat
control equipment
controllability
fins
shape memory alloys
Radiators
graphite
engineering
requirements
Hot Temperature
Solar absorbers
configurations
Graphite
Controllability

Keywords

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

ASJC Scopus subject areas

  • Fluid Flow and Transfer Processes

Cite this

Study on a Reversible Thermal Panel for spacecraft (detailed design based on parametric studies and experimental verification). / Nagano, Hosei; Ohnishi, Akira; Nagasaka, Yuji; Nagashima, Akira.

In: Heat Transfer - Asian Research, Vol. 35, No. 7, 11.2006, p. 464-481.

Research output: Contribution to journalArticle

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