Dual-mode airbreathing propulsion system
AssigneeCU Aerospace, LLC
InventorRodney L. Burton
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AssigneeCU Aerospace, LLC
InventorRodney L. Burton
Estimating the term…
The present invention includes a method for a dual-mode propulsion system. During the first mode of operation, intake air is liquefied through a cooling heat exchanger and condenser using a combination of stored liquid hydrogen (LH2) and stored liquid nitrogen (LN2) as coolants. The liquefied air is then separated into separated liquid oxygen (SLO2) and separated liquid nitrogen (SLN2), which may contain molecules of each other or other elements commonly found in air. The stored liquid nitrogen is replaced with SLO2, while the SLN2 is pumped back through the system with the stored nitrogen in a regeneration process. The SLN2, LN2, and LH2 become gaseous as they pass through the condenser and heat exchanger and are burned in the dual mode rocket thrust chamber to produce thrust. In the second mode, the same thrust chamber is operated as a liquid hydrogen-oxygen rocket, where the liquid oxygen is the SLO2 collected during the first mode.
A method for a dual-mode aerospace vehicle propulsion system comprising:
A system for providing a dual-mode propulsion system comprising:
In a method of performing a first and second mode of propulsion, utilizing a single combustion chamber nozzle assembly, the method comprises:
In a method of performing a first and second mode of propulsion, the method comprises:
Dependencies are inferred from the claim text.