The space station and spacecraft A and B are all in the same circular earth orbit of 350 km altitude. Spacecraft A is 600 km behind the space station and spacecraft B is 600 km ahead of the space station. At the same instant, both spacecraft apply a Dvt so as to arrive at the space station in one revolution of their phasing orbits.
(a) Calculate the time required for each spacecraft to reach the space station.
(b) Calculate the total delta-v requirement for each spacecraft.