An earth satellite traveling in the elliptical orbit shown has a velocity v = 12,149 mi/hr as

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An earth satellite traveling in the elliptical orbit shown has a velocity v = 12,149 mi/hr as it passes the end of the semi minor axis at A. The acceleration of the satellite at A is due to gravitational attraction and is 32.23 [33959/84004]2 = 7.159 ft/sec2 directed from A to O. For position A calculate the values of r˙, r¨, θ˙, and θ¨.

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Engineering Mechanics Dynamics

ISBN: 9781118885840

8th Edition

Authors: James L. Meriam, L. G. Kraige, J. N. Bolton

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