A propellant distributor or anode includes a plenum chamber and a plurality of outlets. The at least one plenum chamber is configured to receive a flow of propellant from an inlet, and the plurality of outlets are configured to distribute the flow of propellant into an inner channel wall and an outer channel wall of a discharge channel.
Propellant distributor for a thruster
2019-04-30
Patent
Elektronische Ressource
Englisch
lon-Thruster Propellant Utilization
AIAA | 1972
|Ion-thruster propellant utilization
TIBKAT | 1971
|