Kepler's 3rd Law and the Doppler Effect

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SUMMARY

The discussion focuses on calculating the mass of a distant planet using Kepler's 3rd Law and the Doppler Effect. The probe emits a radio signal with a wavelength of 8 m, which varies between 7.99943 m and 8.00057 m over a period of 4.5 hours. The key equations used include the Doppler shift formula, Δλ/λ = v/c, and the circular velocity equation, vc = √(GM/a). The participants emphasize the importance of defining variables such as mass (M), velocity (v), and the gravitational constant (G) to solve the problem accurately.

PREREQUISITES
  • Understanding of Kepler's 3rd Law
  • Familiarity with the Doppler Effect
  • Knowledge of gravitational force equations, specifically F = GMm/R^2
  • Basic concepts of circular motion and orbital mechanics
NEXT STEPS
  • Research the Doppler Effect in detail, focusing on its application in astrophysics
  • Study Kepler's 3rd Law and its implications for celestial mechanics
  • Explore gravitational force equations and their relevance to orbital dynamics
  • Learn about the relationship between wavelength shifts and velocity in astrophysical contexts
USEFUL FOR

Astronomy students, astrophysicists, and educators seeking to understand the application of Kepler's laws and the Doppler Effect in calculating planetary masses and analyzing orbital mechanics.

dekoi
Question:

Imagine a space probe has been placed in a circular orbit about a distant planet. The probe emits a continuous radio signal with a wavelength of 8 m. You measure the signal from earth, and find it to have a wavelength that varies regularly between 7.99943 m and 8.00057 m, with a period of 4.5 hours. Assuming that you are in the plane of the probe's orbit, and that you are not moving, calculate the mass of the planet.



This is what I have done...

By substituting into different equations, I end up with the equation:
a = λ / 2pi

Using Kepler's 3rd Law:

P^2 = a^3 / mt

I end up with :

mt= (λ / 2pi)^3(1 / P)^2

However, I do not know why I am given 3 different values for wavelength, should this be applied into the answer or not?
 
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dekoi said:
By substituting into different equations, I end up with the equation:
a = λ / 2pi

You got that the semimajor axis of the orbit was comparable to the wavelength of the radiation? I'd like to see which equations you used to get that result. The only radiation for which that would be true is the gravitational variety.

Try instead using:

\frac{\Delta \lambda}{\lambda}=\frac{v}{c}

and

v_c=\sqrt{\frac{GM}{a}}
 
I just did what my teaching assistant told me to do. I don't think it's correct either.

I'm assuming that "c" is the speed of light.

What is the M? Mass of the planet?
 
And what can I do with that equation for v?
 
dekoi said:
I'm assuming that "c" is the speed of light.

What is the M? Mass of the planet?

Sorry, I forgot to define my variables: M is the planet's mass, v is the velocity relative to your line of sight, vc is the circular velocity of the orbit, \Delta \lambda is the shift in wavelength relative to its rest frame value, \lambda is the rest frame value of the wavelength, c is the speed of light, a is the semimajor axis, and G is the gravitational constant.
 
We haven't learned that much information in order to use those equations. The most we have learned is Kepler's 3rd Law and the Gravitational force equation.

F=GMm/ R^2
 
dekoi said:
We haven't learned that much information in order to use those equations. The most we have learned is Kepler's 3rd Law and the Gravitational force equation.

F=GMm/ R^2

The second equation follows simply from Kepler's Third Law, but you do have to know the first one in order to do the problem. I suggest a google (or PF) search on the doppler effect.
 
Okay, thank you anyway.
 

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