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`K.E.` of an orbiting satellite is `K`. The minimum additional `K.E.` required so that it goes to infinity is

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`K.E.` of an orbiting satellite is `K`. The minimum additional `K.E.` required so that it goes to infinity is
A. `K`
B. `2K`
C. `3K`
D. `K//2`
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1 Answer

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Correct Answer - A
`(KE_(2))/(KE_(1))=(v_(e)^(2))/(v_(0)^(2))`
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