Does Mass Affect the Orbital Velocity of Satellites?

AI Thread Summary
The discussion focuses on the relationship between mass and orbital velocity for satellites in circular orbits around Earth. It establishes that the orbital velocity is derived from the gravitational force acting on the satellite, where the formula v = √(Gm/r) applies. When a second satellite with mass three times that of the first is introduced, it is shown that its orbital velocity remains the same, as mass cancels out in the gravitational equation. The key takeaway is that orbital velocity is independent of the satellite's mass, relying solely on the radius of the orbit and the gravitational constant. This conclusion is supported by mathematical reasoning based on Newton's laws of motion and gravitational force.
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Homework Statement



A science group put in a satellite of mass m kg into a circular Earth orbit of radius r. The orbital velocity it needs to remain in this orbit is v. They now put another satellite into a similar orbit at the same altitude. Its mass is 3 times m. What orbital velocity would it need to be given? Give reasons using mathematical reasoning.

Homework Equations



Newton's law v = 2pi x r/T

The Attempt at a Solution



v^2/r=G m/r^2
Satellite 1:
v=√(G m/r)
Satellite 2:
v=√(G 3m/r)
 
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scientict said:

The Attempt at a Solution



v^2/r=G m/r^2

What does 'm' represent here? Can you derive this formula?

When a body moves with constant v in a circular orbit, the centripetal force is constant and equal to the force due to Earth's gravity on the body. Now you can deduce the correct version of the above formula using this.
 
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