Calculate the minimum velocity necessary to launch a spacecraft
from the surface of the Earth to Neptune taking Earth’s rotation
into account. Ignore the Earth’s obliquity.
I understand what escape velocity is and how to calculate it I’m
wondering how to factor in the Earth’s rotation.
Using Escape velocity with addition of Earth's rotation both on it's own axis & around the sun gives the minimum velocity needed to launch space craft to Neptune.
Explanation:
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