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Use the fact that the orbit of a planet about the Sun is an ellipse, with the Sun at one focus. The aphelion of a planet is its greatest distance from the Sun, and the perihelion is its shortest distance. The mean distance of a planet from the Sun is the length of the semimajor axis of the elliptical orbit. The perihelion of Pluto is 4551 million miles, and the distance from the center of its elliptical orbit to the Sun is 897.5 million miles. Find the aphelion of Pluto. What is the mean distance of Pluto from the Sun? Find an equation for the orbit of Pluto about the Sun.

Short Answer

Expert verified
Aphelion: 6346 million miles, Mean distance: 5448.5 million miles. Orbit equation: \[ \frac{x^2}{5448.5^2} + \frac{y^2}{5376.4^2} = 1 \].

Step by step solution

01

Understand the Problem

You need to find the aphelion (greatest distance from the Sun), the mean distance (semimajor axis), and the equation of the orbit of Pluto. Use the given perihelion, the closest distance to the Sun, and the distance from the center to the Sun.
02

Identify Given Values

Perihelion (closest distance) is given as 4551 million miles and the distance from the center to the Sun is 897.5 million miles.
03

Find the Semimajor Axis

Use the fact that the distance from the center to the focus (Sun) is the same as the difference between the semimajor axis (a) and the distance to the perihelion (r_p). Therefore, we have:\[ a - r_p = 897.5 \text{ million miles} \]Since the perihelion (r_p) is 4551 million miles, solve for the semimajor axis (a):\[ a = 4551 + 897.5 = 5448.5 \text{ million miles} \]
04

Calculate the Aphelion Distance

Aphelion distance (r_a) can be found using the relation:\[ r_a = 2a - r_p \]Substitute the known values:\[ r_a = 2 \times 5448.5 - 4551 = 6346 \text{ million miles} \]
05

Write the Equation of the Orbit

For an ellipse centered at the origin with the semimajor axis a and the semiminor axis b, the foci are located at \( \pm c \). Here, c is given as 897.5 million miles. The relationship \( c^2 = a^2 - b^2 \) must be used to find b.\[ c = 897.5 \rightarrow c^2 = 805052.25 \]\[ a = 5448.5 \rightarrow a^2 = 29685482.25 \]\[ b^2 = a^2 - c^2 = 28880430 \]So, the standard form of the elliptical equation is:\[ \frac{x^2}{5448.5^2} + \frac{y^2}{5376.4^2} = 1 \]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Aphelion
The aphelion is the point in the orbit of a planet where it is furthest from the Sun.
For Pluto, the aphelion can be computed by first finding the mean distance (semimajor axis) and using the perihelion information.
The formula for the aphelion distance \(r_a\) is: \[ r_a = 2a - r_p \]
Here, \(a\) represents the semimajor axis, and \(r_p\) is the perihelion distance.
After substituting in the given values and calculations, we find Pluto's aphelion to be 6346 million miles.
This long distance from the Sun signifies that at aphelion, Pluto receives less solar radiation and experiences much colder temperatures compared to when it is at perihelion.
Perihelion
The perihelion is the point where a planet is closest to the Sun during its orbit.
For Pluto, this closest distance is given as 4551 million miles.
At perihelion, Pluto is much closer to the Sun compared to at aphelion, receiving more solar radiation and potentially experiencing slightly warmer temperatures.
This proximity to the Sun is an important factor in understanding how different parts of Pluto’s orbit can affect its climate and solar energy intake.
Semimajor Axis
The semimajor axis is half of the longest diameter of an ellipse.
It's essentially the average distance from a planet to the Sun.
For Pluto, we calculated this distance by adding the given perihelion distance (4551 million miles) and the distance from the center of the orbit to the Sun (897.5 million miles):\[ a = 4551 + 897.5 = 5448.5 \text{ million miles} \]
Hence, 5448.5 million miles is the semimajor axis of Pluto’s orbit.
This semimajor axis helps in understanding the scale and size of Pluto's elliptical orbit around the Sun.
Elliptical Equation
The elliptical equation represents the path of a planet's orbit.
For an ellipse with the Sun at one focus, we determined key elements such as the semimajor axis (a) and the distance from the center to the focus (c).
Using the relationship \[ c^2 = a^2 - b^2 \], we computed the semiminor axis \(b\).
Here, \[ c = 897.5, \ a = 5448.5 \rightarrow a^2 = 29685482.25 \]
Substituting these values: \[ b^2 = a^2 - c^2 = 28880430 \]
Therefore, the standard form of Pluto's elliptical equation is: \[ \frac{x^2}{5448.5^2} + \frac{y^2}{5376.4^2} = 1 \]
This equation characterizes the two-dimensional shape of Pluto's orbit around the Sun.

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