This presentation discusses ground based proof of concept hardware under development at NASA GSFC to address high heat flux thermal management in silicon substrates. 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.
Micro- and Nano-Scale Electrically Driven Two-Phase Thermal Management
Spacecraft Thermal Control Workshop ; 2016 ; El Segundo, CA, United States
2016-03-21
Sonstige
Keine Angabe
Englisch
Europäisches Patentamt | 2020
|Europäisches Patentamt | 2020
|Electrically driven or partially electrically driven vehicle
Europäisches Patentamt | 2022
|Micro-Scale Avionics Thermal Management
NTIS | 2001
|