Resistojet propulsion systems have characteristics that are ideally suited for the on-orbit and primary propulsion requirements of large spacecraft systems. These characteristics which offer advantages over other forms of propulsion are reviewed and presented. The feasibility of resistojets were demonstrated in space whereas only a limited number of ground life tests were performed. The major technology issues associated with these ground tests are evaluated. The past performance of resistojets is summarized and, looks into the present day technology status is reviewed. The material criteria, along with possible concepts, needed to attain high performance resistojets are presented.
Resistojet Propulsion for Large Spacecraft Systems
1982
32 pages
Report
No indication
English
Resistojet propulsion for large spacecraft systems
NTRS | 1982
|Resistojet systems manned spacecraft applications
AIAA | 1969
|Resistojet and plasma propulsion system technology
AIAA | 1972
|RESISTOJET Propulsion System for Small Satellite
IEEE | 2019
|Free Molecule Micro-Resistojet: Nanosatellite Propulsion
NTIS | 2005
|