Theoretical Investigation of UF₆-Based Plasma Propulsion Using He-Ne Laser Discharge Systems

Electric propulsion systems based on plasma dynamics are gaining increased attention for space exploration due to their high efficiency and specific impulse. This paper proposes a novel theoretical model in which a He-Ne laser discharge system is adapted for plasma generation and electromagnetic acceleration, extending the concept by investigating uranium hexafluoride (UF₆) as a high-energy-density propellant. By comparing the physical characteristics and propulsion parameters of UF₆ with conventional noble gases such as xenon and argon, we evaluate its potential for interplanetary missions. While the use of UF₆ introduces major safety and regulatory challenges, its theoretical benefits in thrust performance, ion mass, and energy yield are significant under controlled conditions.

کلیدواژه ها:

Plasma propulsion ، He-Ne laser ، UF₆ plasma ، electromagnetic acceleration ، gas discharge ، interplanetary travel