Orbiting Satellite Homework Help

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SUMMARY

The discussion focuses on calculating the kinetic energy of a satellite in circular orbit around a planet. The satellite's kinetic energy, K, is derived using the formula K = 1/2 m v^2, where v is the orbital velocity. The correct expression for the velocity is obtained from the gravitational force equation, leading to v^2 = GM/R_2. The key takeaway is to ensure the correct mass is used in the kinetic energy formula, specifically the mass of the satellite (m) rather than the planet's mass (M).

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  • Understanding of gravitational force and orbital mechanics
  • Familiarity with the universal gravitational constant (G)
  • Knowledge of kinetic energy formulas in physics
  • Basic concepts of density and volume calculations
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  • Learn about the relationship between mass, density, and volume in spherical objects
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Students studying physics, particularly those focused on mechanics and gravitational systems, as well as educators seeking to clarify concepts related to satellite motion and energy calculations.

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Homework Statement


A satellite of mass m is in a circular orbit of radius R_2 around a spherical planet of radius R_1 made of a material with density rho. ( R_2 is measured from the center of the planet, not its surface.) Use G for the universal gravitational constant.

Find the kinetic energy of this satellite, K.
Express the satellite's kinetic energy in terms of G, m, pi, R_1, R_2, and p.


Homework Equations



I have found the mass of the planet to be

5Cfrac%7B4%7D%7B3%7D%5Cleft%28R_%7B1%7D%5Cright%29%5E%7B3%7D%7B%5Cpi%7D%7B%5Ccdot%7D%7B%5Crho%7D.gif


The magnitude of the gravitational force on the satellite

7D%7B%5Ccdot%7D%7B%5Cpi%7D%7B%5Ccdot%7D%7B%5Crho%7D%5Cright%29%7D%7BR_%7B2%7D%7B%5E%7B2%7D%7D%7D.gif


and the velocity of the satellite to be

render?infix=sqrt%28G%2A4%2Api%2AR_1%5E3%2Arho%2F%283%2AR_2%29%29.gif






The Attempt at a Solution



I thought I could just plug in the velocity of the satellite and the mass of the planet into the equation

K = 1/2MV^2

When I did that I did not get the correct answer. Can anyone please point me in the right direction I probably skipped a step along the way somewhere
 
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For orbit isn't the condition that

mv2/r = GMm/r2

mv2 = GMm/r

1/2*mv2 = 1/2*GMm/R2

Plug in M from p*volume
 
Your reasoning is valid, just did this problem myself. The most likely error is plugging in the wrong mass in the equation for kinetic energy. Notice that the required mass is listed as m, the mass of the satellite, and not M, the mass of the earth. Use your speed in the formula K = 1/2 m_s v_s^2
 

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