A couple of gravitational problems (kelper's third law)

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SUMMARY

The discussion centers on applying Kepler's Third Law to determine the orbital periods of satellites around Earth and Uranus. The correct period for a satellite at an altitude of 1.6 x 106 m is established as 7.2 x 103 seconds. The radius of a synchronous orbit around Uranus, based on Miranda's parameters, is calculated to be 5.8 x 107 m. Participants emphasize the necessity of using consistent gravitational centers when applying Kepler's law.

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  • Understanding of Kepler's Third Law of planetary motion
  • Familiarity with orbital mechanics and gravitational forces
  • Basic knowledge of unit conversions (e.g., days to seconds)
  • Ability to perform calculations involving exponents and scientific notation
NEXT STEPS
  • Study the derivation and applications of Kepler's Third Law
  • Learn about synchronous orbits and their significance in satellite positioning
  • Explore gravitational forces and their impact on orbital motion
  • Investigate the differences between orbital periods of various celestial bodies
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Astronomy students, physics enthusiasts, satellite engineers, and anyone interested in orbital mechanics and gravitational theory.

Vickyvicksss
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Homework Statement



A satellite is to be placed in orbit about the Earth at an altitude of 1.6 x 10 6m. What will be its period of motion?

The answer is 7.2x 103s

2. The attempt at a solution
Using kelper's third law.

R3 / T2 = R3 / T2

Radius of satellite: 6.38 x 106 + 1.6 x 106 = 7.98 x 106
Radius of earth: 6.38 x 106
Period of satellite: ?
Period of earth: 3.16 x 107

When I plugged these numbers in, I get 4.42 x 107s
I've used the formula before without any problems, so that's not the issue.


3. Homework Statement
Determine the radius of a satellite's synchronous orbit around Uranus. Your very friendly, local astronomer informs you that uranus' moon, Miranda, has an average radius of revolution of 1.24 x 105 km with a period of revolution of 1.4 Earth days.

The answer is 5.8 x 107m

4. The attempt at a solution
Same thing as above, I used kelper's third law.
R3 / T2 = R3 / T2

Radius of Miranda: 1.24 x 105
Radius of satellite: ?
Period of miranda: 1.4 days * 3600 * 24 = 120960s
Period of satellite: (I'm assuming this is period of Uranus?) 2.66 x 109

I plugged these numbers in and I got 9.73 x 107m



Thank you in advance!~~ :)
 
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Vickyvicksss said:
Period of earth: 3.16 x 107
What do you mean by 'period of earth'? Where did you get this number?
Period of satellite: (I'm assuming this is period of Uranus?) 2.66 x 109
Where did you get this number?
 
The correct number to plug into Kepler's law here, given that you have plugged in Earth's radius for one of the Rs, is the orbital period of a satellite at ground level, not the orbital period of the Earth around the Sun. The numbers always must refer to orbital periods and orbital radii around the same gravitational center - the Earth, in this case.

Apart from the satellite, what goes round the Earth that has an orbital radius and period that you could look up?

For the second question, do you know what a synchronous orbit is?
 

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