Analytical Design of a Hybrid Electro-Chemical Thruster

摘要

This paper present the models utilized for the design of a hybrid electro-chemical thruster, utilizing both chemical andelectric energy for propellant acceleration. The motivation and basic characteristics of this concept are presented. A generaltheory for practically feasible hybrid electro-chemical thrusters is developed, and its application is demonstrated inMATLAB. The output is discussed, and it leads to considerations regarding how to manufacture such thruster and how toimprove its performance. The concept shows good potential for applications which require higher thrust than electricthrusters and higher specific impulse than rocket engines.