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.
Development of Advanced Spacecraft Thermal Subsystems
2016
23 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Unmanned Spacecraft , Manned Spacecraft , Spacecraft temperature , Temperature control , Fluid management , Control systems design , Systems analysis , Synthetic aperture radar , Transmitter receivers , Heat flux , Electrohydrodynamics , Gravitational effects , Electrophoresis , Research and development , Design analysis , Feasibility analysis
Development of Advanced Spacecraft Thermal Subsystems
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