- #1
Karol
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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.