A rocket is launched vertical from the surface of the earth of radius R with an initial speed `v`. If atmospheric resistance is neglected, then maximum height attained by the rocket is
A. `(R)/(((2gR)/(2v^(2))-1))`
B. `R((gR)/(2v^(2))-1)`
C. `(R)/(((2gR)/(v^(2))-1))`
D. `R((2gR)/(v^(2))-1)`