Question: Physics A spacecraft deployed into a circular orbit inclined 45 deg at 250 km altitude, needs to change to a polar orbit (i=90 deg) at
Physics
A spacecraft deployed into a circular orbit inclined 45 deg at 250 km altitude, needs to change to a polar orbit (i=90 deg) at the same altitude. What delta-V does this maneuver require? Where is this maneuver performed?
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