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AEROJET GENERAL CO

Overview
  • Total Patents
    2,012
About

AEROJET GENERAL CO has a total of 2,012 patent applications. Its first patent ever was published in 1944. It filed its patents most often in United States, United Kingdom and Canada. Its main competitors in its focus markets basic materials chemistry, machines and organic fine chemistry are THIOKOL CORP, POUDRES & EXPLOSIFS STE NALE and NITROCHEMIE GES MIT BESCHRAENK.

Patent filings per year

Chart showing AEROJET GENERAL COs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Frankel Milton B 78
#2 Karl Klager 66
#3 Archibald Thomas G 43
#4 Gold Marvin H 39
#5 Klager Karl 36
#6 Malik Aslam A 32
#7 Bulman Melvin J 31
#8 Gongwer Calvin A 29
#9 Manser Gerald E 23
#10 Grakauskas Vytautas 22

Latest patents

Publication Filing date Title
CN103796749A Catalyst, gas generator, and thruster with improved thermal capability and corrosion resistance
US2013019850A1 Enhanced radiative transfer and heat recovery for combustion device
US2013019849A1 Waste heat recovery for forced convection biomass stove
WO2011103255A1 Mitigation of orbiting space debris by momentum exchange with drag-inducing particles
WO2010120852A1 Cyclic energetic nitramines desensitized with linear nitramines
WO2010118102A1 Gasdynamic laser supplied by catalytic decomposition for skid or vehicle mounting
WO2010036291A2 Ionic liquid multi-mode propulsion system
WO2009142674A1 Rocket nozzles for unconventional vehicles
EP2238020A2 Propulsion system with movable thermal choke
WO2009091430A1 Propellant and explosives production method by use of resonant acoustic mix process
WO2009032447A1 Multi-functional pulse-divided rocket
US2009218086A1 Heat exchanger for a rocket engine
WO2008157413A1 Cathode heater
US2009044716A1 Slow cook off rocket igniter
US2009230212A1 Pintle-controlled propulsion system with external ring actuator
CA2670598A1 Two-piece aft closure for a rocket motor case
WO2008123868A2 Combined cycle missile engine system
WO2008085189A2 Co-sintered multi-system tungsten alloy composite
US2009071120A1 Combined cycle integrated combustor and nozzle system
US2008092519A1 Core burning for scramjet engines