- #1
athrun200
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1(a) Homework Statement
A spaceship travels in a circular orbit around a planet. It applies a sudden
thrust and increases its speed by a factor f . If the goal is to change the
orbit from a circle to a parabola, what should f be if the thrust points in the tangential direction?
1(b) Is your answer any different if the thrust points
in some other direction? What is the distance of closest approach if the
thrust points in the radial direction?
Homework Equations
Kepler’s laws
The Attempt at a Solution
We know that for circle, ε=0; for parabola ε=1
We also know that [itex]ε=\sqrt{1+\frac{2EL^{2}}{m\alpha^{2}}}[/itex]
So [itex]E=-\frac{m\alpha^{2}}{2L^{2}}[/itex] for ε=0
[itex]E=0[/itex] for ε=1
But I don't know what to do next in order to find the increased factor f