公开(公告)号：US20230271728A1

公开(公告)日：2023-08-31

申请号：US17998483

申请日：2021-09-07

Applicant: Khalifa University of Science and Technology

Inventor： Andrei Ivanovich SHUMEIKO ,  Firas Salah JARRAR ,  Sean Shan Min SWEI

IPC: B64G1/40 ,  F03H1/00

CPC classification number: B64G1/405 ,  F03H1/0006

Abstract: An electrodeless plasma thruster with close ring-shaped gas discharge chamber (1,10) can include a gas discharge chamber (1,10) close ring shaped in fluid communication with a propellant storage system (10,70). An antenna (3,30) can be positioned on the exterior of the gas discharge tube (1,10). A guide tube (2,20) can be coupled with the gas discharge chamber (1,10) at a first end and have a second open end. A magnetic system (7,50) can be positioned on the second end of the guide tube (2,20). The magnetic system (7,50) can be electrically coupled with a power supply. The power supply can be electrically coupled with a power converter (11,80) and a control module (12,90).