Translating and Rotating Cowl Inlet with Retractable Propellant Injection Struts
The invention is an inlet system for a variable geometry transatmospheric air-breathing engine. It incorporates a rotatably translatable cowl provided with a rotating lip used in combination with insertable and propellant injection struts.
Patent Status: U.S. patent(s) 5,214,914 issued.CONTACT:
Mr. E. Chalfin
Phone: (443) 778-7473