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- W2023762534 abstract "The gasdynamic mirror (GDM) fusion propulsion concept utilizes a high density plasma in which the collision mean free path far exceeds the length of the system allowing the plasma to behave much like a fluid with confinement properties described by the gasdynamic laws. The symmetric system characterized by equal mirror ratios at each end (suitable for a power reactor) is not particularly useful as a thruster unless the magnetic fluid at one mirror is so tailored as to not cancel the thrust generated at the opposite end. Clearly, an asymmetric device is more appropriate for a propulsion engine especially when one end can be utilized to direct the escaping charged particles to a direct converter that can be used in conjunction with other energy conversion components to allow the system to be self-sustaining once it is ignited. In this paper we present the relevant analysis that underlies the performance of an asymmetric gasdynamic mirror propulsion device." @default.
- W2023762534 created "2016-06-24" @default.
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- W2023762534 date "1997-07-06" @default.
- W2023762534 modified "2023-09-23" @default.
- W2023762534 title "Asymmetric gasdynamic mirror fusion propulsion concept" @default.
- W2023762534 cites W1499869793 @default.
- W2023762534 doi "https://doi.org/10.2514/6.1997-3068" @default.
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