Numerical optimization of Hall effect thruster with variation in magnetic field

Abstract

In the present study, numerical analyses were conducted to enhance the strength of the magnetic field. While electromagnetic coils and permanent magnets have conventionally been used for this purpose, the study explores the utilization of superconducting magnets, known for their significantly stronger magnetic fields. Through analytical tests on a thruster powered by a 5-kW source at 400 V, and 12.5 A current, computer simulations are conducted using an open-source HallThruster.jl developed using Julia language which gave 1D simulation of plasma properties of Hall effect thruster (HET), along a thrust of 0.687 N was achieved representing a three times greater increase, and specific impulse increasing to 3097 s which is 1.7 times more compared to conventional results, accompanied by improved plasma parameters. Furthermore, to study the particle behavior the Particle In cell (PIC) approach was utilized, from which particle motion due to the magnetic field was achieved. By enhancing the magnetic field, we can significantly boost thrust, unlocking new possibilities for exploring distant planets and conducting long-duration space missions. Utilizing superconducting materials ensures continuous, efficient operation with increased thrust and fewer operating payloads, ultimately enhancing overall spacecraft functionality. This advancement paves the way for future innovations in space exploration and applications.