A comet at its closest approach to the Sun

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SUMMARY

The discussion focuses on a comet's elliptical orbit around the Sun, specifically at its closest approach of 125 x 106 km with a speed of 45.5 km/s. The solution confirms that the comet's orbit is elliptical, and the period of the orbit is calculated using Kepler's laws, resulting in a specific timeframe in years. Additionally, the maximum distance from the Sun is computed and compared to the orbital radii of Neptune and Pluto, which are 4510 x 106 km and 5890 x 106 km, respectively.

PREREQUISITES
  • Understanding of elliptical orbits and Kepler's laws
  • Familiarity with conservation of energy principles in orbital mechanics
  • Basic knowledge of astronomical distances and units
  • Ability to perform calculations involving speed, distance, and time
NEXT STEPS
  • Study Kepler's laws of planetary motion in detail
  • Learn about the conservation of energy in gravitational fields
  • Explore the mathematical derivation of orbital periods
  • Investigate the characteristics of comets and their orbits
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Astronomy students, physics enthusiasts, and anyone interested in celestial mechanics and the dynamics of cometary orbits.

Alexanddros81
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Homework Statement


14.102 A comet at its closest approach is 125 x 106 km from the center of the sun
(between the orbits of the Earth and Venus), where its speed is 45.5 km/s. (a) Show that the
comet has an elliptical orbit around the sun. (b) Determine the period of the orbit in years
(1 year = 365.26 days). (c) Compute the maximum distance between the comet and the sun,
and compare it with the radius of the solar system (the orbital radii of Neptune and Pluto,
the two outermost planets, are 4510 and 5890 x106 km, respectively).

Homework Equations

The Attempt at a Solution



Pytels_Dynamics127.jpg


Pytels_Dynamics128.jpg

[/B]
Can you check my solution?
 

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I checked (c) via conservation of energy and it fits, and (b) fits to c and the given initial conditions, so everything should be right.
 

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