US Patent 7770380 Methods of controlling solid propellant ignition, combustion, and extinguishment

Is a

Patent

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Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

77703800

Patent Inventor Names

Michael Dulligan0

Greg Spanjers0

Hieu Nguyen0

James Lake0

Paul Adkison0

David White0

Date of Patent

August 10, 2010

Patent Application Number

103420030

Date Filed

January 13, 2003

Patent Citations Received

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US Patent 12129814 Thrust vector control for hybrid propellants rocket engine with embedded fluid injection ports

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US Patent 11661907 Vortex hybrid rocket motor

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US Patent 11680543 Extinguishable divert system

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US Patent 11879414 Hybrid rocket oxidizer flow control system including regression rate sensors

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US Patent 11927152 Reaction control vortex thruster system

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US Patent 11952965 Rocket engine's thrust chamber assembly

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US Patent 11952967 Liquid propellant injector for vortex hybrid rocket motor

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US Patent 12060853 Rocket engine with integrated oxidizer catalyst in manifold and injector assembly

...

Patent Primary Examiner

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Timothy D Collins

Patent abstract

An apparatus and method to control ignition, combustion burn rate, extinguishment, and reignition of solid propellant is provided.

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US Patent 7770380 Methods of controlling solid propellant ignition, combustion, and extinguishment

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