Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Thermal baseplates are sized to limit high temperature excursions when spacecraft electronics modules are generating peak thermal loads. Because of relatively high nominal conductivity, at low loads makeup heat is required to maintain acceptable temperatures, adding weight associated with batteries, heaters, and thermal control. Thermal switches are systems that are capable of switching between high and low effective conductivity. These systems have been used to eliminate the need for makeup heaters; however, because these systems are electronically driven they add weight in the form of batteries and thermal control. Contact-aided Cellular Compliant Mechanisms (C3M) employ internal contact mechanisms to enable high effective strains in response to mechanical loads. When active, these contacts also introduce new thermal conductive pathways and, using multiple materials, provide a novel avenue to passive thermal control. This paper is concerned with the development of a structure that exhibits effective variable thermal conductivity through its thickness. The proposed concept consists of compliant cells that deform in response to a temperature gradient, alternately creating and breaking heat conduction paths. Initial results indicate that multiple-material C3M devices have the potential to create a large switch ratio between high-conductivity and low-conductivity modes. Complex heat paths through the geometry and thermal characteristc differences between the metal/ceramic pieces help to increase thermal resistance for the low-conductivity mode and generate higher thermal deformation at targeted points.

Original languageEnglish (US)
Title of host publication54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
StatePublished - 2013
Event54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Boston, MA, United States
Duration: Apr 8 2013Apr 11 2013

Other

Other54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
CountryUnited States
CityBoston, MA
Period4/8/134/11/13

Fingerprint

Spacecraft
Thermal conductivity
Thermal load
Switches
Compliant mechanisms
Hot Temperature
Cermets
Heat resistance
Heat conduction
Thermal gradients
Loads (forces)
Electronic equipment
Temperature
Geometry

All Science Journal Classification (ASJC) codes

  • Architecture
  • Materials Science(all)
  • Aerospace Engineering
  • Mechanics of Materials
  • Mechanical Engineering

Cite this

Stavely, R. L., Lesieutre, G. A., Frecker, M. I., & Adair, J. H. (2013). Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control. In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference [AIAA 2013-1588]
Stavely, Rebecca L. ; Lesieutre, George A. ; Frecker, Mary I. ; Adair, James Hansell. / Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control. 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2013.
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Stavely, RL, Lesieutre, GA, Frecker, MI & Adair, JH 2013, Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control. in 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference., AIAA 2013-1588, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Boston, MA, United States, 4/8/13.

Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control. / Stavely, Rebecca L.; Lesieutre, George A.; Frecker, Mary I.; Adair, James Hansell.

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2013. AIAA 2013-1588.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Stavely RL, Lesieutre GA, Frecker MI, Adair JH. Variable thermal conductivity, contact-aided cellular structures for spacecraft thermal control. In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2013. AIAA 2013-1588