Mission to Pluto

The project aims to assess the viability of using three types of rocket motors, including a hybrid engine, to propel a spacecraft on a mission to Pluto. Initially, orbit analysis will be conducted to optimize the trajectory considering gravitational assists and orbital mechanics. Subsequently, combustion and chemical analysis of the fuel types will be carried out, focusing on solid rocket fuel, liquid rocket fuel, and hybrid engines. Solid rocket fuel, prized for its simplicity and reliability, will be evaluated for its thrust capabilities and efficiency over the vast distance to Pluto. Liquid rocket fuel, known for its higher specific impulse and controllability, will be examined for its potential in long-duration missions and course corrections. The hybrid engine, combining elements of solid and liquid propulsion, will be scrutinized for its ability to balance thrust and efficiency for interplanetary travel. Through this comprehensive analysis, the project aims to identify the most suitable propulsion system for the ambitious voyage to Pluto.