– This study aims to present a method for conceptual design and simulation of hybrid propellant motors.
– The design methodology is based on previous studies and thermo-physical governor relations, and also a computational code that was derived to simulate the performance of designed system.
– Conceptual design algorithm for space hybrid propellant systems and method of performance simulation are findings of this study.
– Results of this study are applicable for design process of space systems with hybrid propulsion. Also, simulation results can help the users to improve the performance weaknesses.
– This study shows the implementation of present algorithm for a specified space mission and also study on variation of performance parameters.
