Please help with this problem.   Consider a spacecraft in a 500 km altitude circular orbit.  This spacecraft transits (via Hohmann transfer) to a 200 km altitude circular orbit for repair, then back to a 500 km circular orbit.  Did it require more delta-V to transfer from the higher to lower orbit, or from the lower to higher orbit?  (Circle one) It required more delta-V to transit from 500 km (circular) to 200 km (circular) It required more delta-V to transit from 200 km (circular) to 500 km (circular) It requires the same delta-V to transit from 500 km to 200 km as it would to return There is not enough information to answer this question (if so what other information is missing?)

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Consider a spacecraft in a 500 km altitude circular orbit.  This spacecraft transits (via Hohmann transfer) to a 200 km altitude circular orbit for repair, then back to a 500 km circular orbit.  Did it require more delta-V to transfer from the higher to lower orbit, or from the lower to higher orbit?  (Circle one)

  1. It required more delta-V to transit from 500 km (circular) to 200 km (circular)
  2. It required more delta-V to transit from 200 km (circular) to 500 km (circular)
  3. It requires the same delta-V to transit from 500 km to 200 km as it would to return
  4. There is not enough information to answer this question (if so what other information is missing?)
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