What is the mathematical relationship between the escape velocity (Ve) and the orbital velocity (Vo) of a satellite revolving very close to the surface of the Earth? MCQ with Answer and Explanation

What is the mathematical relationship between the escape velocity (Ve) and the orbital velocity (Vo) of a satellite revolving very close to the surface of the Earth?
A. Vo = sqrt(2) * Ve
B. Ve = 2 * Vo
C. Ve = sqrt(2) * Vo
D. Ve = Vo
Answer: Option C
Solution (By JKExamLibrary)
The orbital velocity of a satellite very close to Earth is Vo = sqrt(gR). The escape velocity from Earth's surface is Ve = sqrt(2gR). Therefore, substituting Vo into the escape velocity equation yields Ve = sqrt(2) * Vo. A satellite requires a 41.4% increase in speed to escape orbit completely.

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