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gcfve
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Homework Statement
Consider a spherical, nonrotating planet of mass M, and radius R, with no atmosphere. A satellite is fired from the surface of the planet with speed v0 at 45o from the local vertical. In its subsequent orbit the satellite reaches a maximum distance of 5R/3 from the centre of the planet. Use conservation of energy and angular momentum to find vo in terms of G, M, R.
Homework Equations
E=[tex]\frac{1}{2}[/tex]mvr2+L2/2mr2+V(r)
The Attempt at a Solution
so far all I have is a=GM/R^2, which I probably don't even need.