Find a relation between orbital velocity of a satellite near the surface of a planet and escape velocity
from the surface of the planet.
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Answer:
1/2 mv² = √ 2GM/r
Explanation
Due to Gravity , The orbiting object will be pulled towards the center of the planet and provide the acceleration to continue drifting in a circular path . Due to this , the object will gain certain velocity and stability when it is at a distance from the center of the planet .
Fg = Fc
= GMm / r² = mv² / r
Orbital velocity ,
V = √ GM/r
The speed at which the kinetic energy of an object is equal to its gravitational potential energy is : -
1/2 mv² = GMm / r
Rearranging to solve for escape velocity ,
Hence the relation ; Ev = √ 2 GM / R
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Answer:
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