公开(公告)号：WO2023037138A1

公开(公告)日：2023-03-16

申请号：PCT/IB2021/058145

申请日：2021-09-07

Applicant: KHALIFA UNIVERSITY OF SCIENCE AND TECHNOLOGY

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

IPC: F03H1/00 ,  B64G1/40

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).