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A satellite revolving close to earth has a K.E., E. What energyshould be given to it so make it escape the gravitational pull of earth? |
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Answer» `(E )/(2)` `E.=(1)/(2)mv_(e )^(2)=(1)/(2)m(sqrt(2)v_(0))^(2)=2((1)/(2)mv_(0)^(2))` `therefore E.=2E` `therefore ` Additional energy to be given `=E.-E=2E-E=E` Thus correct choice is (b). |
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