A rocket of mass M is launched vertically from the surface of the earth with an initial speed V. Assuming the radius of the earth to be R and negligible air resistance, the maximum height attained by the rocket above the surface of the earth is
△K.E.=△U
⇒12MV2=GMeM(1R−1R+h)....(i)
Also g=GMeR2
On solving (i) and (ii) h=R(2gRV2−1)