What is the Gravitational Force on Two Satellites Circling Earth?

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AI Thread Summary
The discussion focuses on calculating the gravitational force on two satellites, A and B, orbiting Earth, with A having ten times the mass of B but B being at a distance one-tenth that of A from Earth's center. The gravitational force decreases with the square of the distance, leading to the equation F = G(m1*m2)/r^2 being crucial for the solution. The user seeks guidance on how to approach the problem, emphasizing the need to determine the forces F_A and F_B and their ratio F_A/F_B. The key takeaway is that understanding the relationship between mass and distance is essential for solving gravitational force problems. This discussion highlights the importance of applying the correct gravitational formula in satellite dynamics.
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Homework Statement



Image attached. This figure shows the force on a 0.1-kilogram mass at various distances from Earth. Notice that the force decreases as the square of the distance. Now, consider satellites A and B, both circling Earth. If A has ten times the mass of B but B is 1/10 of the distance to the center of Earth as is A, what is the gravitational force on A relative to that of B due to Earth?
1/100 times as much
100 times as much
1/10 the amount
10 times as much
the two are equal


Homework Equations


G=m_1*m_2/ r^2



The Attempt at a Solution


I used my textbook and numerous notes and could not figure out a wAy to attempt this problem. Any pointers would be great.
 
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The relevant equation is not $$ G = \frac {m_1 m_2} {r^2} $$ It is $$ F = G \frac {m_1 m_2} {r^2} $$

Now, let ## M ## be the mass of the Earth, ## m_A ## be the mass of A, ## m_B ## the mass of B, ##r_A## and ##r_B## the distances from the Earth to A and B, respectively. What is ##F_A## and ##F_B##? What is ##F_A/F_B##?
 
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