When a body of mass m is undergoing a circular motion of radius r around a body of mass M, the variation of the force of gravitation (F) with distance (r) is given as F = GMmrn
Then, the variation of the time period (T) with orbital distance (R) for a circular orbit will be
(A) TR n                (B) TR –n                  (C) T∝R (n + 1)/2                (D) T∝R (n – 1)/2

Dear student
In the question the force is not clearly shown. Since the force is always inversely proportional to the distance 'r' then we will assume the force as F=GMmrn
Now in the case of circular motion -
gravitational force = mass x centripetal acceleration ,   therefore
 GMmrn=mv2ror, v2=GMr-(n-1)The time period of rotation T, of the circular path is given byT=2πrv=2πrGMr-(n-1)=2πGM r-(n-1)2-1 =2πGM r-(n+1)2Or, T α rn+12option C is correct
I hope it will help you
regards

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