Ratio Problem Dealing with Radius and Centripetal Acceleration

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Homework Help Overview

The problem involves two identical satellites orbiting the Earth, with one satellite traveling at a speed less than that of the other. The original poster is attempting to determine the relationship between the radius of the orbit and the speed of the satellites, referencing centripetal acceleration and gravitational force.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • The original poster expresses confusion about manipulating the relevant equations and questions how the radius relates to the speed of the satellites. Some participants question the understanding of the equations and the implications of stable orbits.

Discussion Status

The discussion is ongoing, with participants providing guidance on the fundamental concepts of gravitational force and stable orbits. There is a recognition of the need for clarification on the relationships between the variables involved.

Contextual Notes

Participants are navigating through the implications of Kepler's Laws and the definitions of stable orbits, indicating potential gaps in understanding the underlying physics principles.

PeachBanana
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Homework Statement



Two identical satellites orbit the Earth in stable orbits. One satellite orbits with a speed v at a distance r from the center of the earth. The second satellite travels at a speed that is less than v . At what distance from the center of the Earth does the second satellite orbit?


Homework Equations


a = (v)^2/r
F = m/a
F = G (M * m )/ r^2

The Attempt at a Solution



I'm really confused on how to manipulate these equations.

Ultimately, I need to find an equation that relates "r" to "v."
r = a * v^2
So if the second satellite is moving slower doesn't that mean "r" has to be bigger? This makes me think of one of Kepler's Laws.
 
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F = m/a
That should read F=ma or a=F/m

What does satellites orbit the Earth in stable orbits tell you about the system?
I'm not sure you understand what you're actually doing when you're working with these equations
 
Wow. That was really careless of me. When it comes to problems like these, I don't understand how to do them well. Stable orbits = equal gravitational force?
 
What should the gravitational force equal?

What does it mean if the orbit is stable?
 

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