The present invention provides a multimode propulsion system, comprising at least one propellant ejector system, a high speed fluid ejection nozzle coupled to a propellant supply provided in the engine, and a propellant-air mixing system comprising at least one fluid intake member having an inlet end and an outlet end, the inlet end being in fluidic communication with the fluid ejection nozzle to receive the propellant ejected from the nozzle.
MULTI-MODE PROPULSION SYSTEM
MULTIMODALES ANTRIEBSSYSTEM
SYSTÈME DE PROPULSION MULTIMODE
2024-05-15
Patent
Electronic Resource
English
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