Determine the necessary amount v by which the circular-orbit velocity of satellite C should be reduced if
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Determine the necessary amount Δv by which the circular-orbit velocity of satellite C should be reduced if the catch-up maneuver of Prob. 3/288 is to be accomplished with not one but two periods in a new elliptical orbit.
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Related Book For 
Engineering Mechanics Dynamics
ISBN: 9781118885840
8th Edition
Authors: James L. Meriam, L. G. Kraige, J. N. Bolton
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