Background:The development of efficient propulsion systems for space exploration remains a significant challenge,particularly for deep space missions. Tokamaks, known for their ability to generate high-energyplasma and sustain controlled fusion reactions, could theoretically provide the necessary thrust forinterplanetary and interstellar travel. This paper explores the concept of utilizing Tokamak reactors,typically designed for nuclear fusion research, as a propulsion system for spacecraft.Material and methods:The methodology involves analyzing the principles of plasma dynamics, magnetic confinement, andenergy conversion from a Tokamak reactor to a directed exhaust for propulsion.Results:Theoretically, while the Tokamak-powered propulsion system technology is still in its early stages,a Tokamak-powered propulsion system could potentially achieve higher specific impulse than traditional chemical rockets even if significant challenges in magnetic confinement, plasma stability, andheat management might remain. Computational simulations are worth being conducted to modelthe performance of a Tokamak-based rocket engine, considering factors such as energy output, fuelefficiency, and thrust-to-weight ratio.Conclusion:In conclusion, while promising, the Tokamak rocket propulsion concept requires further research andtechnological advancement to become a viable alternative to current space propulsion systems.