1.

Energy required to move a body of mass 'M' from an orbit of radius 2R to 3R is........

Answer»

`(GM)/(12R)`
`(GMm)/(3R^(2))`
`(GMm)/(8R)`
`(GMm)/(6R)`

SOLUTION :Change in P.E in displacing a body from `r_(1)and r_(2)` is given by :
`DeltaU = GMm [1/(r_(1))-1/(r_(2))]= GMm [1/(2R) -1/(3R)] = (GMm)/(6R)`


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