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Information about assignment 6 for astronomy 345, due on october 10, 2008, with partial credit until october 17, 2008. The assignment includes problems based on hartmann's textbook and supplemental problems related to identifying kirkwood gaps in main belt asteroids and deriving expressions for orbital velocities in elliptical orbits. Students are required to use kepler's laws and perform integrals to find the results.
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Astr 345 Assignment 6
Due before midnight Fri, Oct 10, 2008 (full credit), before midnight Fri Oct 17, 2008 (half credit)
(a) Starting with Kepler’s 2nd law, derive the following expression for the angular velocity of an object in an elliptical orbit in terms of orbital parameters:
vθ =
2 πa P
1 + e cos θ √ 1 − e^2
(b) Starting with the polar equation for the ellipse, show that the radial velocity of an object in an elliptical orbit is: vr = 2 πa P
e sin θ √ 1 − e^2 (c) Using the above two expressions, verify the vis-visa equation from v^2 = v^2 r + v^2 θ.
< f (t) >=
τ
∫ (^) τ
0
f (t)dt.
Beginning with the expression for the integral average, prove that
< U >= −G
M μ a
You may use the following integral: ∫ (^2) π
0
dθ 1 + e cos θ
2 π √ 1 − e^2
HINT: you will have to transform the integral from one of dt to one of dθ using Kepler’s 1st and second laws.
Grading: