The shuttle orbiter A is in a circular orbit of altitude 200 mi, while spacecraft B is
Chapter 2, Problem 2/202(choose chapter or problem)
The shuttle orbiter A is in a circular orbit of altitude 200 mi, while spacecraft B is in a geosynchronous circular orbit of altitude 22,300 mi. Determine the acceleration of B relative to a nonrotating observer in the shuttle A. Use for the surface-level gravitational acceleration and mi for the radius of the earth. 2/202
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