1.

If orbit velocity of planet is given by v = G^(a)M^(b)R^(c), then

Answer»

`a = (1)/(3),b=(1)/(3),c=-(1)/(3)`
`a=(1)/(3),b=(1)/(2),c=-(1)/(2)`
`a=(1)/(2), b=-(1)/(2),c=(1)/(2)`
`a=(1)/(2),b=-(1)/(2),c=-(1)/(2)`

SOLUTION :`v=sqrt((GM)/(R))=G^(1//2)M^(1//2)R^(-1//2)`


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