Philip P. answered 02/12/18
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Let R be the Earth's radius and M be its mass. The gravitational force on a rocket of mass m at the surface is:
F = GMm/R2
where G is the Gravitational Constant. The acceleration is F/m = GM/R2. Let the rocket be at a height h above the surface. Its distance from the Earth's Center (of mass) is R + h. We want:
GM/(R+h)2 = (1/2)GM/R2
Solving for h:
2R2 = (R+h)2
(√2)R = R + h
(√2)R - R = h
(√2 - 1)R = h
(0.414)R ≅ h
Note that the result is independent of the rocket's mass, m.