Asked by Abidur
Derive an expression for escape speed of satellite.
Answers
Answered by
bobpursley
KE needed=PE at origin
1/2 m v^2=GMe*m/distance
"escape speed of satellite" would depend on escape from what, I assume you are trying to get it out of orbit into deep space. https://en.wikipedia.org/wiki/Escape_velocity
1/2 m v^2=GMe*m/distance
"escape speed of satellite" would depend on escape from what, I assume you are trying to get it out of orbit into deep space. https://en.wikipedia.org/wiki/Escape_velocity
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