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: C
Solution :
Orbital velocity of satellite \[{{v}_{0}}=\sqrt{\frac{GM}{R}}\] ?(i) and escape velocity of satellite \[{{v}_{e}}=\sqrt{\frac{2GM}{R}}\] ..(ii) Hence, \[{{v}_{e}}=\sqrt{2}{{v}_{0}}\]You need to login to perform this action.
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