Gravitation Energy: Calculating Required Energy for Orbit w/ m, T, M, R

In summary: Therefore, the first and second terms in my solution do not add up to the second term in the book's solution.
  • #1
Karol
1,380
22

Homework Statement


A mass m is sent from Earth into an orbit. the period is T.
What is the energy required to put it into orbit. express it with T, m, M, R(radius of earth)

Homework Equations


$$E=\frac{1}{2}mv^2-\frac{GMm}{r}$$
$$2\pi r=vT$$

The Attempt at a Solution


I expressed the radius of the orbit r and the velocity:
$$r=\sqrt[3]{\frac{GMT^2}{4\pi^2}}$$
$$v=\sqrt[3]{\frac{2\pi GM}{T}}$$
Those results are correct according to the book. the energy required:
$$E=\frac{1}{2}mv^2-\frac{GMm}{r}-\left(-\frac{GMm}{R}\right)$$
$$E=m\frac{\sqrt[3]{\frac{4\pi^{2}G^{2}M^2}{T^2}}}{2}-GMm\left(\sqrt[3]{\frac{4\pi^2}{GMT^2}}-\frac{1}{R}\right)$$
$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{3}M^{3} 4\pi^2}{GMT^2}}+\frac{GMm}{R}$$
$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{2}M^{2} 4\pi^2}{T^2}}+\frac{GMm}{R}$$
The answer in the book is:
$$E=GMm\left( \frac{1}{R}-\sqrt[3]{\frac{\pi^2}{2GMT^2}}\right)$$
I can reach to that form, but this answer includes only the first:
$$\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}$$
And the last elements in my result.
 
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  • #2
ff

I solved it using the energy in an orbit:
$$E=-\frac{GMm}{2r}$$
 
  • #3
Karol said:

Homework Statement


A mass m is sent from Earth into an orbit. the period is T.
What is the energy required to put it into orbit. express it with T, m, M, R(radius of earth)

Homework Equations


$$E=\frac{1}{2}mv^2-\frac{GMm}{r}$$
$$2\pi r=vT$$

The Attempt at a Solution


I expressed the radius of the orbit r and the velocity:
$$r=\sqrt[3]{\frac{GMT^2}{4\pi^2}}$$
$$v=\sqrt[3]{\frac{2\pi GM}{T}}$$
Those results are correct according to the book. the energy required:
$$E=\frac{1}{2}mv^2-\frac{GMm}{r}-\left(-\frac{GMm}{R}\right)$$
$$E=m\frac{\sqrt[3]{\frac{4\pi^{2}G^{2}M^2}{T^2}}}{2}-GMm\left(\sqrt[3]{\frac{4\pi^2}{GMT^2}}-\frac{1}{R}\right)$$
$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{3}M^{3} 4\pi^2}{GMT^2}}+\frac{GMm}{R}$$
$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{2}M^{2} 4\pi^2}{T^2}}+\frac{GMm}{R}$$
The answer in the book is:
$$E=GMm\left( \frac{1}{R}-\sqrt[3]{\frac{\pi^2}{2GMT^2}}\right)$$
I can reach to that form, but this answer includes only the first:
$$\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}$$
And the last elements in my result.
The first and second terms of your solution can be added together and are identical to the second term of the books solution.
 
  • #4
dauto said:
The first and second terms of your solution can be added together and are identical to the second term of the books solution.
My solution:
Karol said:
$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{2}M^{2} 4\pi^2}{T^2}}+\frac{GMm}{R}$$
The answer in the book is:
$$E=GMm\left( \frac{1}{R}-\sqrt[3]{\frac{\pi^2}{2GMT^2}}\right)$$
It's not true that the first and second terms of my solution make the term in the book:
$$m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{2}M^{2} 4\pi^2}{T^2}}=\frac{1}{8}m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{T^2}}-64m\sqrt[3]{\frac{G^{2}M^{2} \pi^2}{T^2}}=-63\frac{7}{8}m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{T^2}}$$
And the term in the book gives:
$$GMm\sqrt[3]{\frac{\pi^2}{2GMT^2}}=m\sqrt[3]{\frac{G^{3}M^{3}\pi^2}{2GMT^2}}=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}$$
And it's only the first term in my answer
 
  • #5
What I am doing wrong?

Your approach is correct, but there is a small error in your final equation. It should be:

$$E=m\sqrt[3]{\frac{G^{2}M^{2}\pi^2}{2T^2}}-m\sqrt[3]{\frac{G^{2}M^{2} 4\pi^2}{T^2}}+\frac{GMm}{R}$$

Notice the exponent on the second term should be 2, not 3. This will give you the same result as the book's answer.

In addition, you can simplify your final equation to:

$$E=\frac{GMm}{R}-m\sqrt[3]{\frac{2G^2M\pi^2}{T^2}}$$

This may make it easier to see where your error was. Keep in mind that the final answer is not unique, as long as it includes the terms $\frac{GMm}{R}$ and $\sqrt[3]{\frac{2G^2M\pi^2}{T^2}}$.
 

FAQ: Gravitation Energy: Calculating Required Energy for Orbit w/ m, T, M, R

1. What is gravitation energy?

Gravitation energy is a form of potential energy that results from the gravitational attraction between objects. It is the energy required to move an object against the force of gravity.

2. How is gravitation energy calculated?

Gravitation energy can be calculated using the formula E = -GMm/R, where G is the gravitational constant, M and m are the masses of the two objects, and R is the distance between them.

3. What is required energy for orbit and how is it calculated?

The required energy for orbit is the amount of energy needed for an object to maintain a stable orbit around another object. It can be calculated using the formula E = -GMm/2R, where G is the gravitational constant, M and m are the masses of the two objects, and R is the distance between them.

4. How does mass, time, and distance affect gravitation energy?

The greater the mass of the objects, the greater the gravitation energy. The longer the time that the objects are in close proximity, the greater the gravitation energy. The greater the distance between the objects, the lower the gravitation energy.

5. Can gravitation energy be converted into other forms of energy?

Yes, gravitation energy can be converted into other forms of energy, such as kinetic energy, when an object falls towards a larger object due to the force of gravity. It can also be converted into potential energy when an object is moved to a higher distance from the larger object.

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