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Q.1.A satelite of mass m revolving in circular orbit of radius r round the earth of mass M has a total energy E.The angular momentum of the satelite will be .................
Q.2.Two satelite P1 and P2 are revolving in orbits of radii R and 4R. The ratio of maximum to minimum angular velocities of the line joining P1 and P2 is ..............
((please solve it for me))
using kepler's third law:
T2= 8T1
but T2= 2pi (4r)/ V2
similarly T1
we get, V1=2V2
but w= V/R
hence, i get W1 : W2 = 8 : 1
reply me if it is correct.
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