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
2017-10-03
Patent
Electronic Resource
Russian
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2017