Applied-Field Magnetoplasmadynamic Thrusters for Deep Space Exploration
Matthew Han, Hannah Rana

TL;DR
This paper reviews recent progress in Applied-Field Magnetoplasmadynamic Thrusters (AF-MPDTs), highlighting technological advancements, challenges, and the path toward spaceflight readiness for deep space exploration.
Contribution
It provides an in-depth analysis of AF-MPDT technology, including recent developments in superconducting coils, cryocoolers, and thermal management, and discusses the steps needed for operational deployment.
Findings
TRL 4-5 achieved by prototypes
Cryocoolers at 40 K enable HTS integration
Thermal control and power supply are key challenges
Abstract
Recent advancements in the development of Applied-Field Magnetoplasmadynamic thrusters (AF-MPDTs) present themselves to be an increasingly promising propulsion technology for deep space exploration missions. Various entities, ranging from state-sponsored institutions to privately-owned startups, have developed AF-MPDTs across a wide range of power levels. Current developments in superconducting technologies, namely High-Temperature Superconducting (HTS) coils such as REBCO, have enabled research into the integration of HTS coils into the applied-field module to generate MPD thrust. Developments in space cryocoolers have opened the doors for HTS use within a spaceflight design of an AF-MPDT, where the applied-field module is at 40 K. A TRL of 4-5 has been reached by some AF-MPDT prototypes; venturing beyond this will require higher cooling power space cryocoolers to be developed in…
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Taxonomy
TopicsMagnetic confinement fusion research · Particle accelerators and beam dynamics · Plasma Diagnostics and Applications
