What is the Velocity of a Satellite Orbiting Earth at a Distance R?

AI Thread Summary
To determine the velocity of a satellite orbiting Earth at a distance R from its center, the gravitational force must be equated to the centripetal force. The correct formula involves using the gravitational constant G and the mass of the Earth, leading to the expression v = sqrt(G*M/R). It's important to note that the acceleration due to gravity is not constant at large distances, and the variable R should indeed be included in the final answer. The discussion emphasizes the need to apply the full Newtonian gravitational force equation rather than simplifying it incorrectly. Overall, the derived formula is valid and reflects the necessary physics for satellite motion.
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Homework Statement


Find the velocity of a satellite which circles the Earth at a distance R from the Earth's centre.

Homework Equations


Fc = (m*v^2)/r
W = mg

The Attempt at a Solution


I put Fc = W (I think I can do that?)
so (v^2)/R = g
v = sqrt(10R)

I'm not sure if my answer is right or if I'm supposed to actually work out with R is. Can anyone help?
 
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g is not constant over large radial distances. The assumption of constant g also assumes that the physics is taking place 'near the Earth's surface'.

Instead of using W = mg, use the full expression for the Newtonian force due to gravity.
 
Hi.

Use this relation:

F = G*m*M/d²

Here: - m is the mass of satellite.
- M is the mass of the Earth.
- d is the distance between the center of the Earth and the Satellite.
- G is the gravitationnal constant.

Warning for the distance ;) !

Good Luck.
 
Fg = Gm1m2/d^2
I think I can just use one m since the mass of the Earth is very large realtive to the satellite.
so Fg = Gm/R^2
put Fg = Fc
and I get v= sqrt(G/R)
where G is the gravitational constant

I presume I'm supposed to have the variable R in my answer since they didn't give it in the question?
 
dvvv said:
Fg = Gm1m2/d^2
I think I can just use one m since the mass of the Earth is very large realtive to the satellite.

No, m1 and m2 are multiplied, not added. A small number multiplied by a much larger number is an even larger number.

Also consider the units of the equation. While F = G*m1*M2/r2 is a force, G*m1/r2 is not -- it's an acceleration (because F/m2 is an acceleration by Newton's second law). But this is a big clue! You can calculate the acceleration due to gravity of the satellite. What other acceleration is operating here to balance it?

I presume I'm supposed to have the variable R in my answer since they didn't give it in the question?

That's right.
 
g = G*M/R^2
centripetal acceleration a = (v^2)/R
g = a
I get v = sqrt(G*M/R)

:confused:
 
Don't be confused, that's a perfectly fine result!
 
Ok, thanks for your help. :)
 
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