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PHY-2024-CT3-049
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PHY · PHY-2024-CT3-049
Physics
Section B
The minimum energy required to launch a satellite of mass m from the surface of earth of mass M and radius R in a circular orbit at an altitude of 2R from the surface of the earth is
A
GmM/(2R)
B
GmM/(3R)
C
5GmM/(6R)
D
2GmM/(3R)
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