Suppose the orbit of a planet is an ellipse of eccentricity e = c/a and period T

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Suppose the orbit of a planet is an ellipse of eccentricity e = c/a and period T (Figure 2). Use Kepler’s Second Law to show that the time required to travel from A to B is equal to

A' e (+) a B 0 B' b T Sun (c, 0)

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Calculus

ISBN: 9781319055844

4th Edition

Authors: Jon Rogawski, Colin Adams, Robert Franzosa

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