Hohmann Transfer Calculator

Calculates the parameters necessary for an orbital transfer between two coplanar circular orbits using the principles of astrodynamics. The tool determines the minimum energy trajectory, known as a Hohmann transfer, which involves applying two impulsive burns to move a spacecraft from its initial orbit radius to a target orbit radius. It computes critical values such as the required change in velocity at both points and the total characteristic energy needed for the mission profile. Astrodynamics students, amateur space enthusiasts, and preliminary mission designers utilize this calculator to model theoretical interplanetary or orbital maneuvers. Users can determine the most fuel-efficient path between two defined orbits without requiring complex manual calculations involving orbital mechanics equations.