1.

In a satellite if the time of revolution is T, then K.E. is proportional to                     [BHU 1995]

A.             \[\frac{1}{T}\]
B.             \[\frac{1}{{{T}^{2}}}\]
C.             \[\frac{1}{{{T}^{3}}}\]      
D.             \[{{T}^{-2/3}}\]
Answer» E.


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