A) \[\frac{GmM}{2{{(R+h)}^{2}}}\]
B) \[\frac{GmM}{4{{(R+h)}^{2}}}\]
C) \[\frac{GmM}{2(R+h)}\]
D) \[\frac{GmM}{4(R+h)}\]
Correct Answer: C
Solution :
\[{{E}_{i}}=-\frac{GMm}{2(R+h)}\] \[{{E}_{f}}=-\frac{GMm}{2(R+h)}\] So energy required to remove the satellite from gravitational influence of earth is\[\frac{GMm}{2(R+h)}\]You need to login to perform this action.
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