Prove that if a planetary orbit is circular of radius R, then vT = 2R, where v is the
Chapter 13, Problem 9(choose chapter or problem)
Prove that if a planetary orbit is circular of radius R, then vT = 2R, where v is the planets speed (constant by Exercise 7) and T is the period. Then use Keplers Third Law to prove that v = k R
Unfortunately, we don't have that question answered yet. But you can get it answered in just 5 hours by Logging in or Becoming a subscriber.
Becoming a subscriber
Or look for another answer