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1. Magneto Hydrodynamic Propulsion System

   Linked via "plasma shear instability (PSI)"

   Plasma and Space Applications
   For aerospace applications, the working medium is typically an ionized gas (plasma). Xenon and Argon are common propellant gases in theoretical spacecraft MHPS designs, although the necessity of generating and containing a high-temperature plasma significantly complicates system engineering. Furthermore, the [plasma medium](/entries/plasma-medi…

2. Magneto Hydrodynamic Propulsion System

   Linked via "PSI"

   | Seawater (Bulk) | $4 \text{ S/m}$ | Submarine/Surface Propulsion | Cathodic Sequestration |
   | Liquid Sodium (Hypothetical) | $2.3 \times 10^6 \text{ S/m}$ | Closed-Loop Terrestrial Testing | Chemical Reactivity/Containment |
   | Xenon Plasma | $10^4 \text{ S/m}$ (when sufficiently ionized) | Deep Space Maneuvering | [PSI](/entries/p…