Gravitation - Period of revolution of planet

AI Thread Summary
The discussion centers on calculating the period of revolution for a planet orbiting the Sun using Kepler's laws. Participants clarify that the semi-major axis is represented as (r+R)/2 and discuss the relationship between the orbital period and the mass of the Sun, not the planet. The correct formula for the period is derived as T = π√((r+R)³/(2GM)), emphasizing that the mass M refers to the Sun. There is consensus that the period remains unaffected by the planet's mass, as it only depends on the Sun's mass and the semi-major axis. The conversation concludes with participants confirming their understanding and reaching the correct answer.
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Homework Statement


A planet of mass ##M## moves around the Sun along an ellipse so that its minimum distance from the Sun is equal to ##r## and the maximum distance is ##R##. Making use of Kepler's laws, find its period of revolution.

(Ans: ##\pi \sqrt{(r+R)^3/(2GM)}##)

Homework Equations


Kepler's laws:
1. The orbit of every planet is an ellipse with the Sun at one of the two foci.
2. A line joining a planet and the Sun sweeps out equal areas during equal intervals of time.
3. The square of the orbital period of a planet is proportional to the cube of the semi-major axis of its orbit.


The Attempt at a Solution


From the third law, ##T^2 \propto R^3## but according to the answer there should be a ##(r+R)^3## and also, I don't know how would I determine the constants here.

Any help is appreciated. Thanks!
 
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Pranav-Arora said:
Kepler's laws:
...
3. The square of the orbital period of a planet is proportional to the cube of the semi-major axis of its orbit.

The attempt at a solution[/b]
From the third law, ##T^2 \propto R^3##

Does ##R## represent the semi-major axis?
 
TSny said:
Does ##R## represent the semi-major axis?

Silly me, it is ##(r+R)/2##, correct now?

What about the constants? :confused:
 
Pranav-Arora said:
Silly me, it is ##(r+R)/2##, correct now?
Yes.

What about the constants? :confused:

Not sure what you are asking here.
 
TSny said:
Not sure what you are asking here.

We have ##T^2 \propto (r+R)^3/8 \Rightarrow T^2=k(r+R)^3/8##. How do I determine k here?
 
Note that the formula for the period does not depend on the eccentricity of the ellipse when the period is expressed in terms of the semi-major axis. So, the constant factor will be the same for all elliptical orbits. Pick a value of eccentricity that would make the analysis simple.
 
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TSny said:
Note that the formula for the period does not depend on the eccentricity of the ellipse when the period is expressed in terms of the semi-major axis. So, the constant factor will be the same for all elliptical orbits. Pick a value of eccentricity that would make the analysis simple.

How about eccentricity be zero? :P

Thank you TSny! I have reached the correct answer. :)
 
Pranav-Arora said:

Homework Statement


A planet of mass ##M## moves around the Sun along an ellipse so that its minimum distance from the Sun is equal to ##r## and the maximum distance is ##R##. Making use of Kepler's laws, find its period of revolution.

(Ans: ##\pi \sqrt{(r+R)^3/(2GM)}##)
Where M is the mass of the planet? Doesn't sound right. If you doubled the mass of the planet, wouldn't it follow the same path and have the same period?
 
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haruspex said:
Where M is the mass of the planet? Doesn't sound right.

I think you are right, shouldn't that be the mass of Sun? :confused:
 
  • #10
It should be the mass of the Sun.

ehild
 
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  • #11
Yes, Thanks haruspex and ehild. I didn't even notice that M was given as the mass of the planet.
 
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