Development of Advanced Spacecraft Thermal Subsystems

Didion, Jeffrey R.

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NASA NTRS · 20160006931

Development of Advanced Spacecraft Thermal Subsystems

Didion, Jeffrey R.

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Abstract

This presentation discusses ground based proof of concept hardware under development at NASA GSFC to address high heat flux thermal management in silicon substrates and embedded thermal management systems. The goal is to develop proof of concept hardware for space flight validation. The space flight hardware will provide gravity insensitive thermal management for electronics applications such as transmit/receive modules that are severely limited by thermal concerns.

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BibTeX RIS

Didion, Jeffrey R.. 2016-05-31. Development of Advanced Spacecraft Thermal Subsystems. https://ntrs.nasa.gov/citations/20160006931

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