An artificial satellite revolves around a planet for which gravitational force(F) varies with distance r from its centre as F is directly proportional to r^2. If v' its orbital speed , then
a)v' directly proportional to r^-1/2
b)v'directly proportional to r^3/2
c)v'directly proportional to r^-3/2
d)v'​directly proportional to r

Orbital Speed = GMr
So ,
v' directly proportional to r^-1/2

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