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.
СХОДЯЩЕЕСЯ/РАСХОДЯЩЕЕСЯ МАГНИТНОЕ СОПЛО
03.10.2017
Patent
Elektronische Ressource
Russisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Europäisches Patentamt | 2017