Solving Kepler's Equation for Comet Orbit Time Around Sun

In summary, to find the time it takes for a comet to make its orbit around the sun, you can use the equation T^2/R^3 = K, where K is the Kepler's constant (3.36x10^18). Since the comet is 10 times farther from the sun than the Earth, the ratio of their distances can be set as 1:10, making the ratio of their times 1:31.6 (T_{comet}=31.6T_{earth}). Therefore, the time it takes for the comet to make its orbit around the sun is approximately 31.6 times longer than the time it takes for the Earth.
  • #1
susan__t
20
0

Homework Statement



A comet is 10 times farther from the sun than the Earth. Find the time it take to make its orbit around the sun.

Homework Equations


T^2/R^3 = K
K= 3.36X10^18


The Attempt at a Solution



I tried to create a ratio, but I honestly have no idea where to start. I'm not even sure I need to know kepler's constant for this problem. and the answer is T=31.6

I don't know what to put as R, and that leaves me with two variables, R and T.
I also don't know if Kepler's constant is the same for the comet and the earth.
 
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  • #2
since k is equal for both objects, you can set each objects time^2/distance^3 ratio equal to each other. Then use that [tex]R_{comet}=10R_{earth}[/tex].
 
  • #3


I would approach this problem by first understanding the fundamental principles behind Kepler's equation and its application to celestial bodies in orbit around the sun. Kepler's equation is a mathematical formula that relates the orbital period (T) of a celestial body to its distance from the sun (R). The constant K in the equation represents the combined mass of the sun and the celestial body, and it is the same for all objects in orbit around the sun.

In this case, we are given that the comet is 10 times farther from the sun than the Earth. Therefore, we can express the distance of the comet from the sun as 10 times the distance of the Earth from the sun, or 10R (where R is the distance of the Earth from the sun). We can also express the orbital period of the comet as T (since that is what we are trying to find).

Substituting these values into Kepler's equation, we get:

T^2/(10R)^3 = K

Simplifying this equation, we get:

T^2/1000R^3 = K

Since we know the value of K (3.36x10^18), we can rearrange the equation to solve for T:

T^2 = 1000R^3 x 3.36x10^18

Taking the square root of both sides, we get:

T = √(1000R^3 x 3.36x10^18)

Now, we need to determine the value of R. We know that the distance of the Earth from the sun (R) is approximately 149.6 million kilometers. Therefore, the distance of the comet from the sun (10R) would be 149.6 million kilometers x 10, or 1.496 billion kilometers.

Plugging this value of R into the equation, we get:

T = √(1000 x (1.496 billion)^3 x 3.36x10^18)

Simplifying this, we get:

T = √(1.496^3 x 1000 x 3.36x10^18) x 10^9

T = √(7.113 x 10^27) x 10^9

T = 2.666 x 10^19 seconds

Converting this to years, we get:

T = 846,330,000 years

 

What is Kepler's Equation?

Kepler's Equation is a mathematical formula developed by Johannes Kepler to describe the motion of planets and other objects in our solar system. It relates an object's orbital period (time to complete one orbit) to its distance from the Sun and the mass of the Sun.

Why is it important to solve Kepler's Equation for comet orbit time around the Sun?

Comets are celestial bodies that can have highly elliptical orbits around the Sun, and accurately predicting their orbit time is crucial for understanding their behavior and predicting when they will be visible from Earth. Solving Kepler's Equation allows us to accurately calculate the orbital period of a comet and make predictions about its future movements.

What are the variables involved in Kepler's Equation?

The variables in Kepler's Equation are the orbital period (P), the semi-major axis (a), and the mass of the central body (M). The semi-major axis is the distance from the center of the ellipse to one of its foci, and the mass of the central body is typically the mass of the Sun in the case of objects orbiting around it.

How do scientists solve Kepler's Equation for comet orbit time around the Sun?

There are several methods for solving Kepler's Equation, including analytical methods, numerical methods, and graphical methods. One common approach is to use numerical methods, such as Newton's method, to iteratively solve the equation and find the value of the orbital period.

What are some real-world applications of solving Kepler's Equation for comet orbit time around the Sun?

Aside from predicting the motion of comets, solving Kepler's Equation has many practical applications. It is used in spacecraft trajectory planning, satellite orbit calculations, and even in the study of exoplanets. By accurately predicting the motion of objects in space, we can better understand our solar system and the universe around us.

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