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

In summary, the satellite circles the Earth at a distance of 10,000 kilometers. Its velocity is calculated to be 8,000 kilometers per hour.
  • #1
dvvv
26
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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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  • #2
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.
 
  • #3
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.
 
  • #4
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?
 
  • #5
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.
 
  • #6
g = G*M/R^2
centripetal acceleration a = (v^2)/R
g = a
I get v = sqrt(G*M/R)

:confused:
 
  • #7
Don't be confused, that's a perfectly fine result!
 
  • #8
Ok, thanks for your help. :)
 

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

What is the definition of velocity of a satellite?

The velocity of a satellite is the measure of its speed and direction of motion in relation to a fixed point, typically the Earth's surface.

How is the velocity of a satellite calculated?

The velocity of a satellite is calculated using the formula v = √(GM/R), where G is the gravitational constant, M is the mass of the central body (such as the Earth), and R is the distance between the satellite and the central body.

How does the velocity of a satellite affect its orbit?

The velocity of a satellite determines the shape and size of its orbit. A higher velocity will result in a larger orbit, while a lower velocity will result in a smaller orbit.

Can the velocity of a satellite change?

Yes, the velocity of a satellite can change due to various factors such as atmospheric drag, gravitational forces from other bodies, and propulsion systems on the satellite.

Why is the velocity of a satellite important?

The velocity of a satellite is important because it affects its stability, trajectory, and ability to perform its designated tasks. It also plays a crucial role in determining the amount of time it takes for a satellite to orbit around a planet.

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