Solving Problem 9: Smaller than Any of the Choices?

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The discussion centers on solving a problem related to orbital mechanics, specifically addressing whether a circular orbit assumption is necessary. It clarifies that Kepler's Laws can be applied to both circular and elliptical orbits. Participants confirm that the mass of the planet does not need to be calculated directly. Instead, they discuss using the ratio of R^3 to T^2 based on existing data to derive the necessary values for the problem. The conversation emphasizes the importance of understanding the proportional relationship in orbital dynamics.
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Homework Statement


see problem 9 attachment


Homework Equations


see problem 9 attempt attachment


The Attempt at a Solution


I come up with a solution that is much smaller than any of the choices. I do not know if I am to assume the orbital is circular. I do not know if there is another error besides that in my work.
 

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Hello,

You need not assume that the orbit is circular. Use one of Kepler's Laws (which applies for both circular and elliptical orbits).
 
ok if I use kepler's third law would I start by using moon II orbital period and radius to solve for the mass of the planet?
 
You don't need to solve for the planet's mass. Remember that R^3 is proportional to T^2, and that must hold for all objects orbiting a body. Hence R^3/T^2 = constant.
 
ok so I can find that ratio from moon II data and then multiply that ratio by T^2 of moon III?
 
yup, that is right
 
thank you for your help
 
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