| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 05/17/1992 | CA2055716A1 Wall resisting high thermal gradients and providing large heat flux flow |
| 05/12/1992 | US5111657 Propulsion device comprising a block of propellant provided with a central duct of variable section |
| 05/06/1992 | EP0484209A1 Retractable axial bearing with flexible membrane for a rotary machine |
| 05/06/1992 | EP0483255A1 Lateral thrust assembly for missiles |
| 05/05/1992 | USH1049 Gas generation for a missile post-boost control system |
| 05/05/1992 | US5110047 Vane-type nozzle(s) for varying the magnitude and direction of a thrust vector, and methods of operating same |
| 05/05/1992 | US5109669 Passive self-contained auto ignition system |
| 04/21/1992 | US5107129 Fiber optic solid/hybrid rocket motor grain regression rate sensor |
| 04/15/1992 | EP0480085A1 Gas generator |
| 04/14/1992 | US5103637 Rocket engine combustion chamber |
| 04/14/1992 | CA1298733C Increased range artillery projectile |
| 04/08/1992 | EP0479424A1 A propulsion assembly for an aerospace vehicle ejector seat |
| 04/07/1992 | US5101731 Propellant grain assembly for a gas generator |
| 04/07/1992 | US5101623 Rocket motor containing improved oxidizer injector |
| 04/07/1992 | US5101622 Aerospace propulsion |
| 04/01/1992 | EP0477482A1 Foamed in place igniter and aft-end assembly for rocket motor comprising the same |
| 04/01/1992 | EP0477238A1 Methods and apparatus for cryogenic removal of solid materials |
| 03/31/1992 | US5099764 Propulsion unit fireable from an enclosure |
| 03/31/1992 | US5099645 Liquid-solid propulsion system and method |
| 03/10/1992 | CA1296984C Process for installing liner in pressure vessel |
| 03/05/1992 | DE4027915A1 Pulse-jet aircraft engine - has curved pipe instead of usual floating disc valve for higher thrust with lower weight |
| 02/19/1992 | EP0471605A1 Device for thermal protection of an inner wall of a hollow structure subjected to an ablative gasflow and method for producing the same hollow structure |
| 02/05/1992 | EP0469964A1 Turbopump to simultaneously compress two fluids |
| 02/04/1992 | US5085725 Method of chemical bonding of solid propellant grains to the internal insulation of an interceptor motor |
| 02/04/1992 | US5085343 Nested tank construction |
| 02/04/1992 | US5085041 Dual mode engine having a continuously operated oxidizer pump |
| 02/04/1992 | CA1295428C Ion source |
| 01/21/1992 | US5082202 Droppable jet vane TVC |
| 01/09/1992 | DE4029279A1 Lightweight rocket propulsion aggregate - esp. for helicopter blade tip motor and operation using monergolic and/or hypergolic propellant and catalyst pack |
| 01/08/1992 | EP0442899A4 Vane-type thrust vectoring nozzle |
| 01/07/1992 | USH1007 Solid fuel ramjet combustor |
| 01/07/1992 | US5078336 Spin-stabilized missile with plug nozzle |
| 01/07/1992 | US5077968 Vaneless contrarotating turbine |
| 01/02/1992 | EP0463659A1 Projectile with propellant powder in the form of elongated powder strips |
| 01/02/1992 | EP0463022A1 Pyrotechnic materials. |
| 12/31/1991 | US5075966 Method for fabricating a hollow component for a rocket engine |
| 12/27/1991 | EP0428627A4 Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor |
| 12/24/1991 | US5074762 Compact structural assembly for feeding propellants at high pressure to a rocket engine |
| 12/24/1991 | US5074697 Releasable connector for interconnecting two parts subjected to high stresses |
| 12/24/1991 | US5074492 System for steering a missile by means of lateral nozzles |
| 12/24/1991 | US5074187 Rocket nozzle shield |
| 12/17/1991 | US5072891 Combination actuator and coolant supply for missile and rocket vector control |
| 12/11/1991 | EP0460449A1 Rocket engine |
| 12/10/1991 | US5071093 Liquid propellant supply device for spacecraft adapted to predict the end of its service life |
| 12/10/1991 | US5070691 Solid propellant canister loaded multiple pulsed or staged rocket |
| 12/03/1991 | US5069135 Elongate main propellant powder charges |
| 11/26/1991 | US5067316 Rocket engine expansion nozzle with complementary annular nozzle |
| 11/12/1991 | US5063735 Rocket-powered ducted fan engine |
| 11/12/1991 | US5063734 Method for providing real-time control of a gaseous propellant rocket propulsion system |
| 11/06/1991 | EP0380591A4 Fiber/resin composites, and method of making the same |
| 11/05/1991 | US5062206 Removable rocket motor igniter |
| 10/29/1991 | US5060550 Rocket nozzle snubber |
| 10/29/1991 | US5060470 Having memory metal transformed at temperature below ignition temperature of rocket propellant; preventing bursting from pressure build-up |
| 10/15/1991 | US5056405 Propellant-to-inhibitor bonding system |
| 10/08/1991 | US5054287 Extended temperature range rocket injector |
| 10/01/1991 | US5052176 Combination turbojet-ramjet-rocket propulsion system |
| 09/18/1991 | EP0447284A1 Missile control system by means of lateral gas jets |
| 09/18/1991 | EP0447283A1 Missile control system by means of lateral nozzles |
| 09/17/1991 | US5048289 Extendible nozzle |
| 09/04/1991 | EP0445011A1 Geostationary observation satellite with multi-nozzle liquid propellant apogee manoeuvering system |
| 09/03/1991 | US5044156 Device designed to modify the trajectory of a projectile by pyrotechnical thrusters |
| 09/03/1991 | US5044154 Safety mechanism for rendering a rocket motor non-propulsive |
| 08/29/1991 | DE4040860A1 Jet engine for aircraft - has partition forming inner combustion chambers and outer free-jet chambers with Laval nozzles |
| 08/28/1991 | EP0443371A1 Method to control space thrusters |
| 08/28/1991 | EP0443018A1 Security igniter for propulsor |
| 08/28/1991 | EP0442899A1 Vane-type thrust vectoring nozzle. |
| 08/27/1991 | US5042385 Inhibitor and barrier for use with high energy rocket propellants |
| 08/27/1991 | US5042365 Annular preloaded seal for a sliding piston in cylindrical tank |
| 08/27/1991 | CA2037005A1 Geostationary earth observation satellite incorporating multiple thruster liquid propellant apogee maneuver system |
| 08/14/1991 | EP0441704A1 Rigid and pressure permeable thermal protection device |
| 08/14/1991 | EP0441703A1 Flexible and pressure transmitting thermal protection device |
| 08/13/1991 | US5038561 Thermal insulators for rocket motors |
| 08/06/1991 | US5036658 Pressure relief device for solid propellant motors subjected to high external temperatures |
| 07/30/1991 | US5035112 Non-continuous ignition train |
| 07/16/1991 | US5032201 Method for the production of a combustion chamber for solid propellant rocket motor |
| 07/16/1991 | US5031539 Radiation curable rocket motor liner for case bonded solid propellant |
| 07/10/1991 | CN1052926A Wrapping process for shaping jet tube joint basement of roclcet engine shell made up by wrapping fibre |
| 07/02/1991 | US5027596 High performance propulsion thruster, especially for attitude and orbit control of a space flight body |
| 06/26/1991 | EP0434565A1 Versatile combined propulsion engine for aeroplane or space shuttle |
| 06/26/1991 | EP0434509A1 Liquid propergol supply system for space vehicle capable of predicting its exhaustion |
| 06/25/1991 | US5026259 Miniaturized pressurization system |
| 06/25/1991 | US5025632 Method and apparatus for cryogenic removal of solid materials |
| 06/25/1991 | US5025623 Rocket engine |
| 06/23/1991 | CA2032589A1 Liquid propellant supply device for spacecraft adapted to predict the end of its service life |
| 06/18/1991 | US5024860 Rocket motor insulation using phosphonitrilic elastomeric compositions |
| 06/11/1991 | US5023006 Thermal insulation chemical composition and method of manufacture |
| 06/11/1991 | US5022324 Piezoelectric crystal powered ignition device |
| 06/11/1991 | US5022306 Method of ejecting an interceptor missile from its silo |
| 05/29/1991 | EP0428627A1 Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor. |
| 05/21/1991 | US5016835 Guided missile |
| 05/14/1991 | US5014508 Combination propulsion system for a flying craft |
| 05/14/1991 | US5014507 Direct drive gaseous hydrogen turbo actuator |
| 05/08/1991 | EP0426001A1 Method and device for accelerating the automatic opening of a parachute |
| 05/07/1991 | US5012640 Combined air-hydrogen turbo-rocket power plant |
| 05/02/1991 | EP0425384A1 Method and device to protect the catalytic bed of a thruster from degradation |
| 04/30/1991 | US5010730 Gas-fed hybrid propulsion system |
| 04/30/1991 | US5010728 Solid fuel turbine engine |
| 04/16/1991 | US5007236 Removable rocket motor igniter |
| 04/10/1991 | EP0421865A1 Rocket combustion chamber |
| 04/05/1991 | CA2026430A1 Combustion chamber for a propulsion unit |