A space vehicle is in a circular orbit at an altitude of 362 km above the earth.
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A space vehicle is in a circular orbit at an altitude of 362 km above the earth. To return to earth, it decreases its speed as it passes through A by firing its engine for a short interval of time in a direction opposite to the direction of its motion. Knowing that the velocity of the space vehicle should form an angle φB =60? with the vertical as it reaches point B at an altitude of 64.4 km, determine
(a) The required speed of the vehicle as it leaves its circular orbit at A,
(b) Its speed at point B.
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Related Book For
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073212227
8th Edition
Authors: Ferdinand Beer, E. Russell Johnston, Jr., Elliot Eisenberg, William Clausen, David Mazurek, Phillip Cornwell
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