A space probe describes a circular orbit of radius nR with a velocity v0 about a planet
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A space probe describes a circular orbit of radius nR with a velocity v0 about a planet of radius R and center O.
Show that
(a) In order for the probe to leave its orbit and hit the planet at an angle θ with the vertical, its velocity must be reduced to αv0, where
(b) The probe will not hit the planet if α is larger than √2/(1+n)
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Related Book For
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073398242
11th edition
Authors: Ferdinand Beer, E. Russell Johnston Jr., David Mazurek, Phillip Cornwell, Brian Self
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