Spacecraft propulsion devices and systems with microwave excitation

A multi-mode thruster system for use in a spacecraft includes a microwave source; a cavity coupled to the microwave source and including a first inlet to receive a first fluid and a second inlet to receive a second fluid; and a nozzle provided at one end of the cavity. The thruster operates in a mic...

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Bibliographische Detailangaben
Hauptverfasser: Hummelt, Jason, Sercel, Joel, Parman, Matthew, Small, James, Mainwaring, Philip
Format: Patent
Sprache:eng
Schlagworte:
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