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List of Aerojet patents

Patents where

Current Assignee

Name

Aerojet

Name	Description	Patent Applicant	Current Assignee	Patent Jurisdiction	Patent Number	Date of Patent
‌ US Patent 7797943 Core burning for scramjet engines	Patent 7797943 was granted and assigned to Aerojet on September, 2010 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7797943	September 21, 2010
‌ US Patent 7621429 Piston tank with compound piston for high loading and expulsion efficiency	Patent 7621429 was granted and assigned to Aerojet on November, 2009 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7621429	November 24, 2009
‌ US Patent 7414135 Process for halomethyl ethers of hydroxyiminomethyl quaternary pyridinium salts	Patent 7414135 was granted and assigned to Aerojet on August, 2008 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7414135	August 19, 2008
‌ US Patent 10954892 Liquid propellant rocket engine nozzle with passive condensate cooling	Patent 10954892 was granted and assigned to Aerojet on March, 2021 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10954892	March 23, 2021
‌ US Patent 10330205 Valve assembly with electronic control	Patent 10330205 was granted and assigned to Aerojet on June, 2019 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10330205	June 25, 2019
‌ US Patent RE41898 Process for halomethyl ethers of hydroxyiminomethyl quaternary pyridinium salts	Patent RE41898 was granted and assigned to Aerojet on October, 2010 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	RE41898	October 26, 2010
‌ US Patent 9505532 Pressure-relief vent	Patent 9505532 was granted and assigned to Aerojet on November, 2016 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	9505532	November 29, 2016
‌ US Patent 10309344 Stored pressure driven cycle	Patent 10309344 was granted and assigned to Aerojet on June, 2019 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10309344	June 4, 2019
‌ US Patent 9784545 Rocket motors having controlled autoignition propellant systems	Patent 9784545 was granted and assigned to Aerojet on October, 2017 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	9784545	October 10, 2017
‌ US Patent 9643700 Selectively submersible vessel	Patent 9643700 was granted and assigned to Aerojet on May, 2017 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	9643700	May 9, 2017
‌ US Patent 9291124 Combined cycle integrated combustor and nozzle system	Patent 9291124 was granted and assigned to Aerojet on March, 2016 by the United States Patent and Trademark Office.	Aerojet	Aerojet	United States Patent and Trademark Office	9291124	March 22, 2016
‌ US Patent 7886516 Combined cycle integrated combustor and nozzle system	Patent 7886516 was granted and assigned to Aerojet on February, 2011 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7886516	February 15, 2011
‌ US Patent 8701379 Combined cycle integrated combustor and nozzle system	Patent 8701379 was granted and assigned to Aerojet on April, 2014 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	8701379	April 22, 2014
‌ US Patent 9708227 Method for producing a fragment / reactive material assembly	Patent 9708227 was granted and assigned to Aerojet on July, 2017 by the United States Patent and Trademark Office.	Aerojet	Aerojet	United States Patent and Trademark Office	9708227	July 18, 2017
‌ US Patent 9200596 Catalytically enhanced gas generator system for rocket applications	Patent 9200596 was granted and assigned to Aerojet on December, 2015 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	9200596	December 1, 2015
‌ US Patent 9206820 Inducer with cavitation instability controls to reduce vibrations and radial loads	Patent 9206820 was granted and assigned to Aerojet on December, 2015 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	9206820	December 8, 2015
‌ US Patent 10640432 Ignition system		Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10640432	May 5, 2020
‌ US Patent 10690424 Hypervelocity cannon	Patent 10690424 was granted and assigned to Aerojet on June, 2020 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10690424	June 23, 2020
‌ US Patent 7414144 Preparation of 2S,3S-	Patent 7414144 was granted and assigned to Aerojet on August, 2008 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7414144	August 19, 2008
‌ US Patent 7309803 Clean, High-yield preparation of S,S and R,S amino acid isosteres	Patent 7309803 was granted and assigned to Aerojet on December, 2007 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	7309803	December 18, 2007
‌ US Patent 10266458 Propellant with extended storage life	Patent 10266458 was granted and assigned to Aerojet on April, 2019 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10266458	April 23, 2019
‌ US Patent 10337457 Rocket motor with energetic grain having region with energetic disposed therein	Patent 10337457 was granted and assigned to Aerojet on July, 2019 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10337457	July 2, 2019
‌ US Patent 9079807 End-burning propellant grain with area-enhanced burning surface	Patent 9079807 was granted and assigned to Aerojet on July, 2015 by the United States Patent and Trademark Office.		Aerojet	United States Patent and Trademark Office	9079807	July 14, 2015
‌ US Patent 9788459 Thermal stand-off with tortuous solid-wall thermal conduction path	Patent 9788459 was granted and assigned to Aerojet on October, 2017 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	9788459	October 10, 2017
‌ US Patent 10883448 Solid rocket motor with vortex inducing feature	Patent 10883448 was granted and assigned to Aerojet on January, 2021 by the United States Patent and Trademark Office.	Aerojet Rocketdyne	Aerojet	United States Patent and Trademark Office	10883448	January 5, 2021

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