Q. An artificial satellite is moving in a circular orbit around the Earth. The height of the satellite above the surface of Earth is R. Suppose the satellite is stopped suddenly in its orbit and allowed to fall freely. On reaching Earth, its speed will be

A) $\sqrt{gR}$
B) $2\sqrt{gR}$
C) $3\sqrt{gR}$
D) 5$\sqrt{gR}$
Explanation

(a) Using conservation of energy.
$\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \frac{1}{2}{mv}^{2} - \frac{GMm}{R} = 0 - \frac{GMm}{2R}$
$or\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \frac{1}{2}{mv}^{2} = \frac{GMm}{R} - \frac{GMm}{2R}$
$or\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ v^{2} = 2\frac{GM}{R}\left\lbrack 1 - \frac{1}{2} \right\rbrack$
$or\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ v^{2} = \frac{GM}{R}\ \ \ $
$But\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ {gR}^{2} = GM$
$\therefore\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ v = \sqrt{\frac{{gR}^{2}}{R}}$
$or\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ v = \sqrt{gR}$

Dr. Abubacker
Reviewed by Dr. Abubacker

Physics Educator & NEET/JEE Specialist

Ph.D. in Physics with 19+ years of teaching experience.

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