Answered: 6.29 At point A on its earth orbit, the… | bartleby

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6.29 At point A on its earth orbit, the radius, speed, and flight path angle of a satellite are rA = 12,
756km, VA =
%3D
6.5992 km/s, and YA
= 20°. At point B, at which the true anomaly is 150°, an
impulsive maneuver causes Av = +0.75820km/s and Av, = 0.
(a) What is the time of flight from A to B?
(b) What is the rotation of the apse line as a result of this maneuver?
{Ans.: (a) 2.045 h; (b) 43.39° counterclockwise}

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