- #1
Lorna
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I am sorry for posting this problem again. I posted it in introductory physics and someone mensioned it might not be an introductory physics problem. Any way I still don't have an answer to it so thought of asking you all, thanks.
A satellite is in circular orbit of radius r about the Earth (Radius R, mass M). Astandard clock C on the satellite is compared with an identical clock C0 at the south pole on Earth. Show that the ratio of the rate of the orbiting clock to that of the clock on Earth is approximately:
1+(GM/Rc^2)-(3GM/2rc^2).
Note that the orbiting clock is faster only if r > 3/2 R, ir if r-R>3184 km.
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The formula to find the rate is : 1+delta (potential)/c^2
so I have to find the diffrence between the potential
potential on Earth = -GM/R
potential of object in orbit = -GM/r
diffrence = GM/R-GM/r
answer should be : GM/R-3GM/2r --- so my answer is wrong
Homework Statement
A satellite is in circular orbit of radius r about the Earth (Radius R, mass M). Astandard clock C on the satellite is compared with an identical clock C0 at the south pole on Earth. Show that the ratio of the rate of the orbiting clock to that of the clock on Earth is approximately:
1+(GM/Rc^2)-(3GM/2rc^2).
Note that the orbiting clock is faster only if r > 3/2 R, ir if r-R>3184 km.
Homework Equations
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The formula to find the rate is : 1+delta (potential)/c^2
so I have to find the diffrence between the potential
The Attempt at a Solution
potential on Earth = -GM/R
potential of object in orbit = -GM/r
diffrence = GM/R-GM/r
answer should be : GM/R-3GM/2r --- so my answer is wrong