Experiments have been carried out in order to study the effectiveness of th
e heat pipe in cooling high dissipative components which are integrated in
Avionics Electronic Modules (AEM). The results show that heat pipes elimina
te hot spots and spread very well the heat dissipated from the components.
The experiments, which are carried out with a real AEM, allow for determini
ng order of magnitude of heat-source/heat sink thermal resistances useful f
or heat pipe integration design and fabrication. The numerical tool develop
ed on the basis of the experimental results allow for the optimization and
better integration of the heat pipe into the AEM.