MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION
MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION
- Neue Suche nach: GANAPATHY ROHAN M
- Neue Suche nach: NOWAL VINOD
- Neue Suche nach: GANAPATHY ROHAN M
- Neue Suche nach: NOWAL VINOD
The present invention relates to a Microwave Electrothermal Thruster(MET) adapted for in-space electrothermal propulsion comprising a tunable frequency Microwave Electrothermal Thruster propulsion module enabling primary propulsion and altitude control of a satellite/spacecraft wherein RF Semiconductors is introduced for the first time as microwave generator inside cavity body to increase its efficiency and respond time and to make the thruster capable of operating in two frequencies by mechanically tuning its cavity making such thruster compact and light weight. The free-floating plasma within the resonant cavity couples the incident electrical power directly to the tangentially injected propellant gas. The plasma forms by focusing the microwave energy into the first transverse magnetic mode and operates independent of the type of propellant gas used. Also, for the first time, Shape Memory Alloy is introduced into the thruster cavity to enable faster and effective tuning of the resonant cavity diameter, when switching between two operational frequencies.
Dokumentinformationen
MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION
2018-11-15
Patent
Elektronische Ressource
Englisch
Ähnliche Titel
Microwave electrothermal thruster adapted for in-space electrothermal propulsion
| Europäisches Patentamt | 2020
A MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION
| Europäisches Patentamt | 2017
A MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION
| Europäisches Patentamt | 2019
Microwave Electrothermal Thruster Performance
| Online Contents | 2007
Microwave Electrothermal Thruster Power
| Online Contents | 1998