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

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SUMMARY

The velocity of a satellite orbiting Earth at a distance R from the Earth's center can be derived using Newton's law of universal gravitation and centripetal force equations. The correct formula for the orbital velocity is v = sqrt(G*M/R), where G is the gravitational constant and M is the mass of the Earth. The assumption of constant gravitational acceleration is incorrect for large distances, and the gravitational force must be expressed as Fg = G*m*M/d². This discussion clarifies the importance of using the correct variables and understanding the relationship between gravitational force and centripetal acceleration.

PREREQUISITES
  • Understanding of Newton's law of universal gravitation
  • Familiarity with centripetal force equations
  • Knowledge of gravitational constant (G)
  • Basic algebra for manipulating equations
NEXT STEPS
  • Study the derivation of orbital mechanics using Newton's laws
  • Learn about the implications of varying gravitational acceleration with distance
  • Explore the concept of centripetal acceleration in different contexts
  • Investigate the applications of satellite motion in real-world scenarios
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Students studying physics, aerospace engineers, and anyone interested in satellite dynamics and gravitational forces.

dvvv
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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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