公开(公告)号：US20240237185A1

公开(公告)日：2024-07-11

申请号：US18595325

申请日：2024-03-04

申请人： HEFEI INSTITUTES OF PHYSICAL SCIENCE, CHINESE ACADEMY OF SCIENCES

发明人： JINXING ZHENG ,  HAIYANG LIU ,  XIAOLIANG ZHU ,  YUDONG LU ,  MING LI ,  YIFAN DU ,  LEI ZHU ,  ZHUOYAO TANG

IPC分类号： H05H1/28 ,  B64G1/40 ,  F03H1/00 ,  H05H1/54

CPC分类号： H05H1/28 ,  B64G1/413 ,  F03H1/0031 ,  H05H1/54 ,  H05H2242/10

摘要： A high-temperature superconducting plasma thruster system, having variable temperature ranges and being applied in space, is provided. The high-temperature superconducting plasma thruster system includes: a cathode-anode assembly, a high-temperature superconducting magnet system, a supporting and adjusting platform, a power-and-gas supply and cooling system, and an obtaining control system. The cathode-anode assembly is disposed at a center of a ring of the high-temperature superconducting magnet system; the cathode-anode assembly and the high-temperature superconducting magnet system are spatially engaged with each other by the supporting and adjusting platform to form a main body of the thruster system; the power-and-gas supply and cooling system and the obtaining control system are located outside of the main body of the thruster system and are connected to the cathode-anode assembly and the high-temperature superconducting magnet system.