International Journal of Aerospace Engineering / 2016 / Article / Tab 4

Research Article

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

Table 4

Orbital thermal condition for the worst case thermal analysis.

ParameterOrbital thermal condition
Worst coldWorst hot

Solar flux [W/m2]12871420
IR flux [W/m2]227249

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