Mean Orbital Separation Question

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SUMMARY

The discussion centers on calculating the mean orbital separation between a moon and its parent planet, specifically when the moon has a mass one quarter that of the planet, which is twice the mass of Pluto. The period of the moon's orbit is given as 12 days. To find the mean orbital separation, users can utilize the rewritten Period formula P=2π√(a³/GM) to solve for 'a', representing the semi-major axis, which corresponds to the average orbital distance. Helpful resources, including calculators for orbital mechanics, are provided for accurate computation.

PREREQUISITES
  • Understanding of orbital mechanics and gravitational forces
  • Familiarity with the Period formula in celestial mechanics
  • Basic algebra for manipulating equations
  • Knowledge of Pluto's mass for calculations
NEXT STEPS
  • Research the application of Kepler's laws in orbital mechanics
  • Learn how to use online orbital calculators for celestial bodies
  • Study the implications of mass ratios in orbital dynamics
  • Explore the gravitational constant (G) and its role in orbital calculations
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Astronomy students, astrophysicists, and anyone interested in celestial mechanics and orbital calculations will benefit from this discussion.

hulkster1988
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So it was basic to figure out the masses and such, but I'm not exactly sure what the "orbital separation" really is? Can someone enlighten me? Here is the question for reference:

A moon with a mass one quarter that of its parent planet orbits that
planet with a period of 12 days. The mass of the planet is twice that of
Pluto. What is the mean orbital separation of the planet and its moon?

Thanks for any help.
 
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planet = 2Pluto
moon = .25 * 2Pluto = 0.5Pluto
total system mass = 2.5 Pluto

Google for Pluto's mass

Once you have it, you can algebraically re-write the Period formula P=2pi*sqrt(a3)/GM) to solve for a, the semi-major axis, which should equal to your orbital separation in a circular orbit, or your average orbital distance when averaged over longitude rather than time. There's a couple of calculators on this page: http://orbitsimulator.com/formulas/ that will do it for you. The 3rd one is the Period formula, and the 4th one is this formula re-written to solve for "a".
 
Great, thanks a lot ...that link is very helpful
 

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