lgaston99
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Homework Statement
Consider what would happen to the temp of a solar array when a solar spacecraft gets into an eclipse. Distance to the Sun is 1 AU and Fs = 1368 W/m2
Consider an infinitely thin flat panel thermally isolated from the spacecraft . Assume the Specific Heat Capacity is 8.0 Kj/K-m2. Also assume the pamel material has infinite thermal conductivity.
In daylight, the solar array is normally illuminated by the solar radiation, and it quickly reaches equilibrium temp.
Assume panel absorptivity \alpha = 0.84 and it's IR emissivity \epsilon=0.74
(a) Calculate solar panel equilibrium temp under solar normal illumination
(b) Estimate solar panel temp by the end of the longest possible eclipse (71 min)
Homework Equations
for (a) T = (\alpha * Fs) / (4*\epsilon*\sigmaSB) --greek letters not to be superscripted (i.e. [4*e*sigSB])
I have no idea what equations should be used for (b) I have looked at
Q = m*c*\DeltaT
Q = e*sigma*A*\Delta T
Q = (A*\Delta T) / H
The Attempt at a Solution
From my calculations I got that the temp = 287.65K
I am completely lost as to where to begin for the temp at the end of the eclipse. Any help or advice would be greatly appreciated.