Systems, methods and apparatus for propulsion

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle with jacketed or hollow... – With subsequent mixing in main discharge stream in or...

Reexamination Certificate

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C239S127100, C239S131000, C060S257000, C060S260000, C060S267000, C060S266000, C060S039530, C060S200100, C060S204000, C060S220000

Reexamination Certificate

active

07997510

ABSTRACT:
In some embodiments a propulsion system includes a thrust chamber having an inside wall, an expansion nozzle mounted to the thrust chamber and having an interior and having an exterior, a main propellant injector mounted to the thrust chamber to inject a fluid in the interior of the thrust chamber, the fluid comprising oxidizer, fuel and internal film coolant, the internal film coolant ranging from about 1% to about 5% of the fluid, limited coolant tubing circumscribing the exterior of the expansion nozzle to circulate an external coolant, and an injector mounted to the expansion nozzle to inject the external coolant in the interior of the expansion nozzle, the external convective coolant about 2.5% of the fluid. The system operates at lower temperatures while having conventional amounts of thrust, in which the thrust chamber can be made of thin walls of lower cost conventional metals with simple coolant tube construction.

REFERENCES:
patent: 3374954 (1968-03-01), Card
patent: 4055044 (1977-10-01), Dederra et al.
patent: 6052987 (2000-04-01), Dressler
patent: 0916835 (1999-05-01), None
patent: 11-229964 (1999-08-01), None

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