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The discussion centers around the power supply mechanisms for an ion drive used in an airplane, as described in a source from MIT. Participants explore various aspects of the technology, including voltage requirements, potential power supply designs, and comparisons to existing technologies.
Participants express various hypotheses regarding the power supply for the ion drive, with no consensus reached on the specific mechanisms or technologies involved. Multiple competing views remain regarding the feasibility and design of the power supply.
Participants mention specific voltage levels and power supply types without resolving the technical details or assumptions underlying their claims. The discussion reflects a range of experiences and theoretical considerations related to ion propulsion systems.
I suspect some sort of switched mode power supply (SMPS) is used.Mark44 said:I wonder how they powered the thing. At the front is a thin wire at + 20,000V and at the rear is a plate at -20,000V. This isn't feasible for batteries I don't believe, so maybe big capacitors?