Engineering Mechanics: Dynamics (14th Edition)
14th Edition
ISBN: 9780133915389
Author: Russell C. Hibbeler
Publisher: PEARSON
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Chapter 21.3, Problem 34P
The 200-kg satellite has its center of mass at point G. Its radii of gyration about the z′, x′, y′ axes are kz' = 300 mm, kx′, = ky′, = 500 mm, respectively. At the Instant shown, the satellite rotates about the x′, y′, and z′ axes with the angular velocity shown, and its center of mass G has a velocity of vG = {–250i + 200j + 120k} m/ s. Determine the angular momentum of the satellite about point A at this instant.
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Chapter 21 Solutions
Engineering Mechanics: Dynamics (14th Edition)
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