Analytical Solution To Relativistic Rocket Motion In Gravitational Space
Abstract
The present author’s earlier paper deals with motion of a relativistic rocket in vacuum excluding the effects of gravity, however small they may be.The present design is aimed at modifying the equations of motion of a relativistic rocket, hypothetically defined as the one having large velocity entailing inclusion of relativistic effects basing on Special Theory of Relativity and including the gravitational force and are determined herein its propellant expenditure, endurance, burnout velocity, burnout altitude and the highest altitude. Finally a numerical example is cited
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