Research Article

Finite Element Analysis of System-Level Electronic Packages for Space Applications

Table 1

Relevant thermomechanical material properties.

MaterialThermal conductivity (W/m-K)Specific heat (J/kgK)EmissivityDensity (kg/m3)

FR40.27915N/A1820
Polystyrene insulation0.0361200N/A30
Aluminum1778750.12790
White paint0.000017N/A0.99801
Plastic interconnects3.9761500N/A1610
Copper4013850.058933
PVC plate0.199000.85527

Emissivity not specified for materials with minimal thermal radiation.