Calculate minimum change in velocity with apogee of 236 and perigee of 205?

<p>Calculate the minimum change in velocity (delta V or &#8710;V) required for the Space Shuttle to decrease its altitude to 60 miles if it&#8217;sorbiting with an apogee of 236 miles and a perigee of 205 miles above the surface of Earth.<br />Use the rule of thumb that below an altitude of 500 miles, forevery 2 feet per second (fps) change in the orbiting space craft&#8217;s velocity its altitude will change by 1 mile.</p>


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