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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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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