How Do You Derive Kepler's Third Law Using Newton's Law of Gravitation?

  • Thread starter Thread starter petern
  • Start date Start date
  • Tags Tags
    Derive
Click For Summary
SUMMARY

Kepler's Third Law of Planetary Motion, expressed as T^2 = kr^3, can be derived from Newton's Law of Universal Gravitation, Fg = (Gm1m2)/(r^2). The gravitational force provides the necessary centripetal force for circular orbits, leading to the equation (Gm1m2)/(r^2) = (mv^2)/(r). By substituting the velocity equation v = (2πr)/T and simplifying, one can arrive at r^3 = (Gm2T^2)/(4π). The constants G, m1, 4, and π can be combined into a single constant k, confirming the relationship defined by Kepler's law.

PREREQUISITES
  • Understanding of Newton's Law of Universal Gravitation
  • Familiarity with centripetal force concepts
  • Knowledge of circular motion equations
  • Basic algebra for manipulating equations
NEXT STEPS
  • Study the derivation of centripetal force equations
  • Explore the implications of Kepler's Laws in celestial mechanics
  • Learn about the gravitational constant G and its significance
  • Investigate the relationship between orbital period and radius in planetary motion
USEFUL FOR

Students of physics, astrophysics enthusiasts, and anyone interested in the mathematical foundations of planetary motion and gravitational theory.

petern
Messages
89
Reaction score
0
Derive Kepler's Third Law of Planetary Motion from Newton's Law of Universal Gravitation.

I know the Law of Universal Gravitation is Fg = (Gm1m2)/(r^2) and the Third Law of Planetary Motion is T^2 = kr^3


What should I do next?
 
Last edited:
Physics news on Phys.org
Start from here:
The gravitational force of attraction between two masses provides the centripetal force required to keep the mass in a circular orbit.

so that (Gm1m2)/(r^2)=m1(w^2)r
 
Which equation does the m1(w^2)r come from?
 
the centripetal force is given by these equations:
F_C=m\omega^2r = \frac{mv^2}{r}=mv\omega

I just used the first equality
 
We haven't learned about m(w^2)r yet so I don't think that's what we're suppose to use. What is the w? However, we've learned about (mv^2)/r.
 
I think I set (Gm1m2)/(r^2) = (mv^2)/(r). I then plug the equation v = (2*pi*r)/T into the one I previously listed. After that, I cancel m1 out and get r1^3 = (Gm2T^2)/(4*pi). After that I don't know how to get rid of the G, m1, 4, and pi so that I'll end up with the equation T^2 = kr^3.
 
Please help. I don't know what to do.
 
petern said:
I think I set (Gm1m2)/(r^2) = (mv^2)/(r). I then plug the equation v = (2*pi*r)/T into the one I previously listed. After that, I cancel m1 out and get r1^3 = (Gm2T^2)/(4*pi). After that I don't know how to get rid of the G, m1, 4, and pi so that I'll end up with the equation T^2 = kr^3.

Then you have done it! G, m, 4, and pi are all constants. You don't need to get rid of them. They can be rolled up into one constant value that you are calling "k".
 

Similar threads

Replies
2
Views
1K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 7 ·
Replies
7
Views
1K
  • · Replies 8 ·
Replies
8
Views
3K
Replies
6
Views
2K
  • · Replies 18 ·
Replies
18
Views
2K
Replies
5
Views
1K
Replies
6
Views
1K
Replies
9
Views
2K
Replies
19
Views
4K