International Journal of Aerospace Engineering / 2016 / Article / Tab 8

Research Article

On-Orbit Thermal Design and Validation of 1 U Standardized CubeSat of STEP Cube Lab

Table 8

Summary of specific parameters variation for TMM correlation.


Coupling conditionStructure/interface board [W/m2-°C]30.0100.0
External panel/solar cell [W/m2-°C]30.0200.0

Heat dissipationBattery [W]0.60.08

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