A spacecraft is sent from the earth to Jupiter by a Hohmann transfer orbit. (a) What is
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A spacecraft is sent from the earth to Jupiter by a Hohmann transfer orbit.
(a) What is the semi-major axis of the transfer ellipse?
(b) How long does it take the spacecraft to reach Jupiter?
(c) If the spacecraft actually leaves from a circular parking orbit around the earth of radius \(7000 \mathrm{~km}\), find the rocket \(\Delta v\) required to insert the spacecraft into the transfer orbit.
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