Vector Mechanics for Engineers: Statics and Dynamics

11th Edition

ISBN: 9780073398242

Author: Ferdinand P. Beer, E. Russell Johnston Jr., David Mazurek, Phillip J. Cornwell, Brian Self

Publisher: McGraw-Hill Education

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Textbook Question

Chapter 12.3, Problem 12.114P

A space probe is describing a circular orbit of radius nR with a velocity v₀ about a planet of radius R and center O. As the probe passes through point A, its velocity is reduced from v₀ to βv₀, where β < 1, to place the probe on a crash trajectory. Express in terms of n and β the angle AOB, where B denotes the point of impact of the probe on the planet.

Fig. P12.114

Chapter 12.3, Problem 12.114P, A space probe is describing a circular orbit of radius nR with a velocity v0 about a planet of

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Chapter 12.3, Problem 12.112P

Chapter 12.3, Problem 12.115P

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Chapter 12 Solutions

Vector Mechanics for Engineers: Statics and Dynamics

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