A spaceship of mass m1 circles a planet (mass = m2) in an orbit of radius r. How much energy is required to transfer the spaceship to a circular orbit of radius 3R?
A) Gm1m2/(2r)
B) Gm1m2/(3r)
C) Gm1m2/(4r)
D) Gm1m2/(6r)
E) 3Gm1m2/(4r)
Correct Answer:
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