1.

A satellite is revolving in a circular orbit of radius r around the earth. The angular momentum of the satellite is proportional to :

Answer»

r
`sqrt(r )`
`r^((3)/(2))`
`(1)/(sqrt(r ))`

Solution :ANGULAR momentum `L=mv_(0)r=root(m)((GM)/(r ))*r`
`L=root(m)(GMr) rArr L prop sqrt(r )`
So the correct choiceis (B).


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