A plasma propulsion system with no internal electrodes is described. Gas is flowed into an insulated axisymmetric plasma liner. A radio frequency antenna generates an inductive or helicon plasma discharge within the liner. The plasma is accelerated through a converging/diverging magnetic field out of the liner, generating thrust.
Electrodeless plasma thruster
17.03.2016
Patent
Elektronische Ressource
Englisch
Electrodeless plasma thruster design
British Library Conference Proceedings | 2005
|Electrodeless Plasma Thruster Design
AIAA | 2005
|