A magnetic nozzle having a converging/diverging contour shape that converts the thermal energy of a propellant into directed kinetic energy, but uses magnetic fields instead of a physical boundary to direct the flow of particles.
Converging/diverging magnetic nozzle
2016-03-10
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Mass transport in a converging-diverging nozzle
TIBKAT | 1986
|Jet-Fuel Cavitation in a Converging-Diverging Nozzle
AIAA | 2007
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