Assume the Earth to be a uniform sphere of mass M and radius R. Also let the Earth be stationary initially. Assume further that there is all other stellar bodies are very far away so as to have no influence in this problem.
A ball of mass $m$ is to be thrown from the surface of the Earth so that it ultimately ends up moving in a circular orbit at a height $h$ from the surface of the Earth. How should the ball be thrown, as in, what should be its initial velocity and, in particular, what should be the angle $\theta$ of the initial velocity with the radial vector from the Earth's center to its initial position on the surface of the Earth?
My attempt at the solution:
Since the Earth-ball system is isolated, its energy would be conserved. Let the initial speed of the ball be $v_0$ and the final speed be $v_f$. We'll have the following equation:
$$ \frac{1}{2}m v_0 ^2 - \frac{GMm}{R} = \frac{1}{2}mv_f^2 - \frac{GMm}{R+h}$$
Next, we know that when the ball will finally be in circular orbit, the gravitational force will be providing the necessary centripetal acceleration for it to maintain circular motion, which gives us the following equation:
$$ \frac{mv_f^2}{R+h} = \frac{GMm}{(R+h)^2} $$
Besides, since gravity is a central force, the angular momentum of the ball about the center of the Earth will remain conserved, which yields the following equation:
$$ mv_0R \sin(\theta) = mv_f(R+h) $$
That completes setting up three equations for three variables $- v_0, v_f, \theta $. Solving them, we would obtain the following values for each:
$$ v_o = \sqrt\frac{GM(R+2h)}{R(R+h)} $$
$$ v_f = \sqrt\frac{GM}{R+h} $$
$$ \theta = \sin^{-1} \Biggl( \frac{1+\frac{h}{R}}{\sqrt{1+\frac{2h}{R}}} \Biggr) $$
However, it is observed that for $\theta$, the argument of $\sin^{-1}$ is always greater than or equal to one, being one only if $h$ is zero. The proof may be carried out by initially assuming that the argument of $\sin^{-1}$ is less than or equal to one for $h$ greater than or equal to $0$, and solving the inequality will yield that $h$ must be less than or equal to zero. So the only acceptable solution is for $h$ to be zero. This just winds up being the case of throwing the ball with sufficient speed tangentially on the surface of Earth so that it keeps orbiting on the Earth's surface itself. Thus, there is no possible way to just throw a ball so that it ends up in a circular orbit of certain desired radius.
The problem is that I don't see any physical intuition for why this should be true; either that or I am doing something wrong. Any guidance or help would be greatly appreciated!
Answer
This problem has one solution. h=0. Throw the ball horizontally at orbital velocity for your altitude.
If you think about it, one of the rules of orbits is that they must eventually come back to where they were. If you throw a ball and it orbits, it must eventually come back around and hit you in the back of the head.
(Incidentally, every ball you throw enters an elliptical orbit like this, but it typically intersects the ground before it gets interesting)
Since all orbits must pass through the thrower, there is only one circular orbit which can be attained, which is the orbit at the height of the thrower. There are several elliptical ones which will leave the atmosphere before coming around to smack you in the back of the head (ignoring air resistance).
To achieve a circular obit, rockets boost into an elliptical orbit, then do a second burn at apogee to "circularize" the orbit. You need to be able to do this second burn in order to achieve a circular orbit at any altitude other than your present one.
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