Math Problem Statement

The arbitrary division where short-period comets end and long-period comets begin is 200 years.

Using Kepler's third law for bodies orbiting the Sun, calculate the semimajor axes for the orbits of a short-period comet with a period of 151.0 years, and for a long-period comet of 751.0 years.

Solution

To solve this, we will use Kepler's Third Law, which states that the square of the orbital period TT of a body is proportional to the cube of the semi-major axis aa of its orbit around the Sun. Mathematically, this is expressed as:

T2=a3T^2 = a^3

where:

  • TT is the orbital period in years.
  • aa is the semi-major axis in astronomical units (AU).

Step 1: Calculate the semi-major axis for the short-period comet (151 years)

Rearrange Kepler's Third Law:

a=T23a = \sqrt[3]{T^2}

For T=151.0T = 151.0 years:

a=(151.0)23a = \sqrt[3]{(151.0)^2}

Let's calculate that.

Step 2: Calculate the semi-major axis for the long-period comet (751 years)

Similarly, for T=751.0T = 751.0 years:

a=(751.0)23a = \sqrt[3]{(751.0)^2}

I will now calculate both values.The semi-major axes for the orbits of the comets are:

  • For the short-period comet with a period of 151.0 years, the semi-major axis is approximately 28.36 AU.
  • For the long-period comet with a period of 751.0 years, the semi-major axis is approximately 82.62 AU.

These values show that the orbits of long-period comets are much more extended compared to short-period comets.

Would you like more details or have any questions?

Here are 5 related questions:

  1. How does Kepler's third law apply to planets within our solar system?
  2. What is the difference between a comet's perihelion and aphelion?
  3. How does the semi-major axis affect the shape of a comet's orbit?
  4. What are the distinguishing characteristics of short-period versus long-period comets?
  5. How would a comet's orbit change if its period were doubled?

Tip: The semi-major axis is a key factor in determining a comet's speed and how elliptical its orbit is—larger axes correspond to longer orbital paths and lower average speeds.

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Math Problem Analysis

Mathematical Concepts

Astronomy
Orbital Mechanics
Kepler's Third Law

Formulas

Kepler's Third Law: T^2 = a^3
Semi-major axis formula: a = T^(2/3)

Theorems

Kepler's Third Law

Suitable Grade Level

Grades 10-12