The moon has mass M 7.7 1022 kg and radius r 1.7 106 m. Calculate work done needed to launch a 1500 kg spacecraft from its surface to other surface.
W=−ΔU=−(GMm∞−GMmr)=GMmr=6.67⋅10−11⋅7.7⋅1022⋅15001.7⋅106=4.5⋅109 (J)W=-\Delta U=-(\frac{GMm}{\infin}-\frac{GMm}{r})=\frac{GMm}{r}=\frac{6.67\cdot10^{-11}\cdot7.7\cdot10^{22}\cdot1500}{1.7\cdot10^6}=4.5\cdot10^9\ (J)W=−ΔU=−(∞GMm−rGMm)=rGMm=1.7⋅1066.67⋅10−11⋅7.7⋅1022⋅1500=4.5⋅109 (J) . Answer
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