Question: Calculate the minimum v required to place a satellite already in Earths heliocentric orbit (assumed circular) into the orbit of Venus (also assumed circular and

Calculate the minimum ∆v required to place a satellite already in Earth’s heliocentric orbit (assumed circular) into the orbit of Venus (also assumed circular and coplanar with Earth). Consider only the gravitational attraction of the Sun. What time of flight would such a trip take?

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