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Physgeek64
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Homework Statement
The emission of radiation from the Sun’s disc is observed to peak at 0.5 μm wave- length and that from the Moon’s disc at 10.0μm. A heat engine to power a Moon base is to be constructed using radiation collected from the Sun. What is the maximum theoretical efficiency of such an engine? Comment on whether it would be practical to achieve this.
Homework Equations
The Attempt at a Solution
##T\lambda_{max}=constant##
##T_{moon}\lambda_{moon max}=T_{sun}\lambda_{sun max}##
##\frac{T_{moon}}{T_{sun}}=0.05##
##\eta=1-\frac{Q_2}{Q_2}##
##\frac{Q_2}{Q_1}=\frac{T_2}{T_1}##
##\eta=1-0.05=0.95##
does this seem right? I feel like assuming the radiation is the same temperature as the sun is wrong
but i don't know how to relate this all together. Any help would be greatly appreciated. Many thanks
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