Exploring the Use of Tokamaks for Rocket Propulsion: A Novel Approach to Space Travel
Creators
Description
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-energy
plasma and sustain controlled fusion reactions, could theoretically provide the necessary thrust for
interplanetary 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, and
energy 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, and
heat management might remain. Computational simulations are worth being conducted to model
the performance of a Tokamak-based rocket engine, considering factors such as energy output, fuel
efficiency, and thrust-to-weight ratio.
Conclusion:
In conclusion, while promising, the Tokamak rocket propulsion concept requires further research and
technological advancement to become a viable alternative to current space propulsion systems.
Files
Barukcic_Rocket_Propulsion_Causation_2025_Vol_20_No_12_pp_5_II.pdf
Files
(3.6 MB)
Name | Size | Download all |
---|---|---|
md5:5960201eab0856a803cbd29a3712fa6e
|
3.6 MB | Preview Download |
Additional details
Dates
- Accepted
-
2024-12-31