Consider a Martian satellite in a circular orbit about Mars with an orbital radius of 15,000 km. It is desired to lower this satellite to a circular orbit of radius 8,000 km using a Hohmann Transfer. Calculate the total impulse required for this maneuver in m/s.
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Ответ:
7.5 m/'s = change of displacement /time taken =7.5/2=
Explanation:
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