two satellite a and b have masses m and 2m respectively.a is in a circular orbit of radius r and b is in the circular orbit of 2r around the earth. what is tha ratio of their kinetic energy?
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Kinetic Energy of the satellite = 1/2 mv²
Now, Velocity of the satellite can be calcualted as,
mv²/r = GMm/r²
v² = GM/r
when r will be close to the earth, then it can be equal to R.
∴ v² = GM/R
∴ v² = gR
∴ v = √gR
Now, Kinetic Energy = 1/2 × m × gR
= mgR/2
For first satellite,
K.E. = mgR/2
For second satellite,
K.E. = 2mgR/2 = mgR
∴ There ratio = 1/2
Hope it helps.
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