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
2016-07-14
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
Mass transport in a converging-diverging nozzle
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