A) \[{{v}_{o}}=\sqrt{2}{{v}^{e}}\]
B) \[{{v}_{o}}={{v}^{e}}\]
C) \[{{v}_{e}}=\sqrt{2{{v}^{e}}}\]
D) \[{{v}_{e}}=\sqrt{2}{{v}_{o}}\]
Correct Answer: D
Solution :
Orbital velocity of satellite |
(i) |
and escape velocity of satellite |
...(ii) |
Hence, |
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