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JEE PHYSICS MCQ: GRAVITATION

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What is the energy required to launch a m kgm \mathrm{~kg} satellite from earth's surface to a circular orbit at an altitude of 7R7 R? (R=R= radius of the earth)
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Correct option: C
1516mgR\frac{15}{16} m g R
Option C (1516mgR\frac{{15}}{{16}} m g R) is correct because it accurately calculates the energy required to launch the satellite to the specified altitude by considering the change in potential energy.

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