Solving the Low-Thrust Rocket Orbital Trajectory

This book describes a new (2015) analytical solution for a circular orbit trajectory for spacecraft propelled by engines with very low thrust, typically electrically powered spacecraft. The solution is derived, explained in detail, and expanded with several additional equations. The fundamental laws of physics and mathematics of calculus are used to derive the solution.

Example space missions such as a round-trip to Mars, travelling to the Moon, and escaping from the Solar system, are analy...