Keplers Third Law: Showing T^2 ∝ R^3

In summary, by equating the gravitational force and the centripetal force on a planet in a circular orbit, it can be shown that the time taken for one orbit (T) is proportional to the radius of the orbit (R) cubed, or T^2\proptoR^3. This can be derived using basic formulas for circular motion and the expression for gravitational force, F=GMm/r^2.
  • #1
skiing4free
20
0

Homework Statement


By considering the centripetal force which acts on a planet in a cirlar orbit, show that T^2[tex]\propto[/tex]R^3, where T is the time taken for one orbitaround the Sun and R is the radius of the orbit.


Homework Equations


Fc=GMm/r^2
1/2Mv^2=GMm/r^2


The Attempt at a Solution


I showed that F[tex]\propto[/tex]1/d^2 but then could not incorporate R^3 into the equation...
 
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  • #2
Well, you made it clear that you know that the gravitational force IS the centripetal force on the planet, and you have the expression for the gravitational force. What is the formula for the centripetal force on an object? Equate these two formulas.
 
  • #3
skiing4free said:
1/2Mv^2=GMm/r^2

This equation isn't even dimensionally correct,
and KE <> PE.
 
  • #4
davieddy said:
This equation isn't even dimensionally correct,
and KE <> PE.

Thats exactly what i showed, Ek=Epg. (<>, that doesn't make sense?)
 
  • #5
skiing4free said:
Thats exactly what i showed, Ek=Epg. (<>, that doesn't make sense?)

<> means NOT equal to.
Anyway potential energy is -GMm/r.

Even if you had erroneously said KE= PE you could have deduced
T^2 proportional to r^3.
 
  • #6
as was previously said just equate the expressions for the gravitational force and the centripetal force GMm/r^2=m(v^2)/r and play with it a bit then use some basic formulas for circular motion for angular velocity and time period and you will get the expression for T and R with some constants in it. Where did you find this : 1/2Mv^2=GMm/r^2 ?
 
  • #7
Sorry i got really confused with the energy equations this is what i meant to write;

F=(m4[tex]\pi[/tex]^2 r)/T^2

F=GMm/r^2

so

(m4[tex]\pi[/tex]^2 r)/T^2=GMm/r^2

m cancels, left with 4[tex]\pi[/tex]^2 r^3=GMT^2

[tex]\Rightarrow[/tex] r^3[tex]\propto[/tex]T^2
 

FAQ: Keplers Third Law: Showing T^2 ∝ R^3

What is Kepler's Third Law?

Kepler's Third Law, also known as the Harmonic Law, states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (R) of its orbit.

How did Kepler discover this law?

Johannes Kepler, a German astronomer, studied the observations made by his mentor Tycho Brahe, and used mathematical calculations to determine the relationships between the orbital periods and distances of planets from the sun.

What does T^2 ∝ R^3 mean?

This means that the ratio between the squared orbital period and the cubed semi-major axis is a constant for all planets in our solar system. In other words, the further a planet is from the sun, the longer it takes to complete one orbit.

Does this law apply to all planets?

Yes, Kepler's Third Law applies to not just planets in our solar system, but also to moons orbiting planets, and other celestial bodies in our universe.

Why is Kepler's Third Law significant?

Kepler's Third Law helped to establish the heliocentric model of our solar system, where planets orbit the sun, and not the Earth. It also paved the way for further advancements in astronomy and our understanding of the laws of planetary motion.

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