Kepler's 3rd Law: Solving Questions & Math

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SUMMARY

This discussion focuses on the application of Kepler's 3rd Law in astrophysics, specifically addressing the calculation of orbital periods using the formula p² = 4π²/G(M1 + M2) / a³. The user inquires about the necessity of using solar masses for mass values and receives clarification that consistent units must be used throughout calculations. The correct application of the formula yields an orbital period of approximately 1.95 years for the given parameters, while an alternative derived equation for time is also presented, resulting in a period of 1.794 years.

PREREQUISITES
  • Understanding of Kepler's Laws of planetary motion
  • Familiarity with gravitational constant (G = 6.67 × 10^-11 m³ kg^-1 s^-2)
  • Knowledge of unit consistency in scientific calculations
  • Basic algebra and square root operations
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  • Study the derivation and application of Kepler's 3rd Law in different unit systems
  • Learn about the gravitational constant and its implications in astrophysical calculations
  • Explore the two-body problem in celestial mechanics
  • Investigate the significance of mass ratios in orbital dynamics
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Astronomy students, astrophysicists, and anyone interested in celestial mechanics and the mathematical principles governing planetary orbits.

mh8780
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Hello I am studying astro independently and have a question on keplers 3rd law and my math.
I set myself with a few givens with Kepler's laws
My first question is, I remember reading M had to be in solar masses, is this true?
For p^2=4π^2/G(M1+M2)/ a^3
Given: a= 1 AU

m1= .31 M☉(Used Gliese 581)
m2= .00095 M☉ (Used Jupiter)
We all know the gravitational constant is 6.67*10^-11
I plug in everything and get

39.47/6.67*10^-11(.31+.00095) *1^3

39.47/6.67*10^-11(.31095) *1^3

39.47/11.44031908×10^12
This is where I always screw up. In my notes I got 10.31065 I don't know how but after this I did:
39.47/10.31065
3.828
√p^2=√3.828
p=1.95 Years

Otherwise I would have got 12000132.94Also when do I use p^2=a^3/(M1+M2) ?
 
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1) You can use SI units but then the period will not be in years of course.
2) Your equation for Kepler's third law is wrong.
 
mh8780 said:
Hello I am studying astro independently and have a question on keplers 3rd law and my math.
I set myself with a few givens with Kepler's laws
My first question is, I remember reading M had to be in solar masses, is this true?

Not unless you use G expressed in solar masses and 'a' expressed in AUs. Look up the units associated with the value of G in your calculations, and use consistent units accordingly for the other quantities in the formula.

http://hyperphysics.phy-astr.gsu.edu/hbase/kepler.html#c6

For p^2=4π^2/G(M1+M2)/ a^3
Given: a= 1 AU

m1= .31 M☉(Used Gliese 581)
m2= .00095 M☉ (Used Jupiter)
We all know the gravitational constant is 6.67*10^-11
I plug in everything and get

39.47/6.67*10^-11(.31+.00095) *1^3

39.47/6.67*10^-11(.31095) *1^3

39.47/11.44031908×10^12
This is where I always screw up. In my notes I got 10.31065 I don't know how but after this I did:
39.47/10.31065
3.828
√p^2=√3.828
p=1.95 Years

Otherwise I would have got 12000132.94Also when do I use p^2=a^3/(M1+M2) ?

It's always a good idea to show units in your calculations. It avoids a lot of confusion in figuring out what your calculation means.
 
Keplers rule disregards the planet masses, the k value being the same for all (negligable mass) planets.
k = p ² / a ³
No good in this case.
You have given both masses and the distance inbetween.
Ive attached the two body data sheet to follow, finding the orbit time for either body (which is the same for both)
can be found.

The derived equation for finding t directly is more involved :

t = square root ( ( 4 * π² * ( M2 / ( M1 + M2 ) ) * d³ ) / ( G * M2 ) )
or
t = square root ( ( 4 * π² * ( M1 / ( M1 + M2 ) ) * d³ ) / ( G * M1 ) )

Using your data, i get :
t = 1.794 years
 

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