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=-\\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)" . Answer
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