Physics Asked on December 16, 2020
I have a question on the following, pertaining to only parts c and d (b was shown to provide the mass of the asteroid and radius):
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I’m going to define the mass of the asteroid here as $M_A$ and the radius of the asteroid here as $R_A$.
My thought process is as follows:
Which of my assumptions are wrong, and how can I go about tackling this logically? Note, this isn’t homework but an example to enforce my learning. Thanks!
Conservation of energy should work at each step of the way. You have potential energy (a function of $r$) and the kinetic energy. Their sum is always constant. The escape velocity is such that the "final" energy (as $rrightarrow infty$) will be zero - no potential energy, no velocity. The intermediate level (where you are intercepting the satellite while "on your way to infinity and beyond") should correspond to a loss of kinetic energy equal to the gain in potential energy.
By setting the potential energy at infinity = 0 (you can pick any radius, but that is a good convention) you find $$PE = -KE$$ at every altitude.
With this convention, the initial and final energy (sum of KE and PE) would be = 0; and when you take into account the launch spring, with elastic energy EE, then you can say $$PE+KE+EE=0$$
And then all your results should follow.
Answered by Floris on December 16, 2020
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