What is the Gravitational Force on Two Satellites Circling Earth?

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SUMMARY

The gravitational force on two satellites, A and B, circling Earth can be calculated using Newton's law of universal gravitation, represented by the equation F = G * (m1 * m2) / r^2. In this scenario, satellite A has ten times the mass of satellite B, but satellite B is located at one-tenth the distance from the center of Earth compared to satellite A. Consequently, the gravitational force on satellite A relative to satellite B is 100 times greater, as the force decreases with the square of the distance.

PREREQUISITES
  • Understanding of Newton's law of universal gravitation
  • Familiarity with gravitational constant (G)
  • Knowledge of mass and distance in gravitational calculations
  • Basic algebra for manipulating equations
NEXT STEPS
  • Study the implications of gravitational force variations with distance in orbital mechanics
  • Learn about satellite dynamics and how mass affects orbital stability
  • Explore advanced gravitational equations in astrophysics
  • Investigate the effects of gravitational force on multiple bodies in space
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Students in physics, aerospace engineers, and anyone interested in understanding gravitational forces acting on satellites in orbit around Earth.

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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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