Invention Grant
US08875485B2 Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster
有权
微阴极推进器和增加微型阴极推进器推力输出的方法
- Patent Title: Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster
- Patent Title (中): 微阴极推进器和增加微型阴极推进器推力输出的方法
-
Application No.: US13081106Application Date: 2011-04-06
-
Publication No.: US08875485B2Publication Date: 2014-11-04
- Inventor: Michael Keidar , Alexey Shashurin , Taisen Zhuang
- Applicant: Michael Keidar , Alexey Shashurin , Taisen Zhuang
- Applicant Address: US DC Washington
- Assignee: The George Washington University
- Current Assignee: The George Washington University
- Current Assignee Address: US DC Washington
- Agency: Panitch Schwarze Belisario & Nadel LLP
- Main IPC: F03H1/00
- IPC: F03H1/00 ; H05H1/02 ; H05H1/10 ; H05H1/50 ; B64G1/40

Abstract:
A magnetically enhanced micro-cathode thruster assembly for providing long-lasting thrust is provided. The micro-cathode thruster assembly includes a tubular housing, a tubular cathode, an insulator, an anode and a magnetic field. The tubular housing includes an open distal end. The tubular cathode is housed within the housing and includes a distal end positioned proximate the open distal end of the housing. The insulator is in contact with the cathode forming an external cathode-insulator interface. The anode is housed within the housing, proximate the open distal end of the housing. The magnetic field is positioned at or about the external cathode-insulator interface and has magnetic field lines with an incidence angle of about 0 to about 90 degrees and preferably about 4 to about 30 degrees relative to the external cathode-insulator interface.
Public/Granted literature
- US20110258981A1 MICRO-CATHODE THRUSTER AND A METHOD OF INCREASING THRUST OUTPUT FOR A MICRO-CATHODE THRUSTER Public/Granted day:2011-10-27
Information query