| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 04/29/1993 | WO1993008444A1 Tailorable roll-bonded insensitive munitions case |
| 04/29/1993 | WO1993003962A3 Satellite propulsion and power system |
| 04/29/1993 | CA2120155A1 Tailorable roll-bonded insensitive munitions case |
| 04/27/1993 | US5205119 Ejector ramjet |
| 04/20/1993 | US5203844 Multiple payload/failure mode launch vehicles |
| 04/07/1993 | EP0535304A1 Arcjet propulsion unit for a space vehicle |
| 04/06/1993 | US5199459 Controlling fuel supply to thruster engines |
| 03/30/1993 | US5197851 Axial flow turbopump with integrated boosting |
| 03/18/1993 | WO1993005356A1 The initiation of propellants |
| 03/10/1993 | EP0530721A1 Device to increase the heat-transfer between a wall and a heat-exchanger fluid |
| 03/09/1993 | US5191761 Aerospace plane and engine |
| 03/04/1993 | WO1993003962A2 Satellite propulsion and power system |
| 03/04/1993 | DE4132415C1 Ablate layer for combustion chamber walls of rocket propulsion appts. - comprises silicone resin with phenyl gp(s) as matrix, high melting filler and alkaline earth carbonate |
| 03/02/1993 | USH1144 Solid propellant rocket motor with fusible end closure holder |
| 02/23/1993 | US5187932 Stored energy combustor |
| 02/17/1993 | EP0527564A1 Pressurised storage for gases |
| 02/09/1993 | US5185312 Method of producing a catalyst for the decomposition of hydrazine |
| 02/02/1993 | USH1140 Asbestos free adhesive insulation |
| 01/13/1993 | EP0522954A1 Surface tension vessel with multiple output flow |
| 01/12/1993 | US5178922 For protecting wall to be submitted to ablative flow at high temperature, thermally insulative matrix, open-weave woven refractory material provided with meshes, refractory armature in form of fringed mat |
| 01/09/1993 | CA2073262A1 Surface tension tank with multiple delivery rates |
| 01/07/1993 | DE4121338A1 Bi-fuel injector for rocket motor - has diaphragms in buffer vessels coupled to smaller diameter plunger and injection plunger |
| 01/05/1993 | US5176508 Turbopump system for driving a plurality of pumps |
| 12/29/1992 | US5175022 Method of making oxidizer coated metal fuels |
| 12/29/1992 | US5174524 Cooling system for high speed aircraft |
| 12/22/1992 | US5173350 Thermal protection coating comprising a fiber reinforced main layer and an insulative sublayer |
| 12/22/1992 | US5172548 Device for tapping off hot gases from a combustion chamber and injector head equipped with such a device |
| 12/22/1992 | US5172547 Electronic valve control for gas generator outflow |
| 12/15/1992 | US5170623 Hybrid chemical/electromagnetic propulsion system |
| 12/08/1992 | US5170007 Tailorable roll-bonded insensitive munitions case |
| 12/08/1992 | US5169093 Method and device for faster automatic deployment of a parachute |
| 12/02/1992 | EP0516519A1 Selflocking, reversible mechanism for the deployment of a rocket nozzle cone |
| 12/02/1992 | CN1066708A Material and structure of inflammable rocket shell and jet tube |
| 12/01/1992 | CA2069204A1 Self-locking and reversible mechanism for deploying the diverging portion of a rocket engine nozzle |
| 11/24/1992 | US5165229 Thruster sealing system and apparatus |
| 11/19/1992 | DE4115720A1 Thrust nozzle for rocket drive with variable expansion ratio - uses ring-shaped device, and circumferential injection of gaseous liquid medium to detach nozzle flow |
| 11/10/1992 | US5161379 Combustor injector face plate cooling scheme |
| 11/03/1992 | US5160392 Pressure vessels, munitions |
| 11/03/1992 | US5160070 Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor |
| 11/03/1992 | US5159809 Highly adaptable combined propulsion engine for an aircraft or a space-going airplane |
| 10/27/1992 | US5158362 Method for measuring the mass of liquid in a storage tank |
| 10/22/1992 | DE4113272A1 Constant pressure ratio maintenance device for rocket engine - includes lasers cooperating with energy storage grids opened alternately at min. electronic voltage and current settings |
| 10/22/1992 | DE4112929A1 Constant pressure ratio maintenance device for rocket engine - includes additional lasers cooperating with successive flow interception grids in downstream direction for energy leakage recovery |
| 10/22/1992 | DE4112623A1 Fuel tank for rocket motor - is connected to smaller tank which collects residual fuel for further use |
| 10/20/1992 | US5156534 Rotary machine having back to back turbines |
| 10/20/1992 | US5156337 Flexible and pressure-permeable heat protection device |
| 10/20/1992 | CA1308921C Thermally initiated mechanically fired device for providing protection against slow cook-off |
| 10/15/1992 | DE4124491C1 Drive set with gaseous and/or liq. fuel delivery - has annular chamber, whose middle section is divided into several narrow chambers |
| 10/14/1992 | EP0508851A1 Shock absorber for a jet propulsion system |
| 10/14/1992 | EP0508609A2 Modular solid-propellant launch vehicle and related launch facility |
| 10/13/1992 | US5154352 Propelling nozzle for an aircraft engine |
| 10/13/1992 | US5154051 Air liquefier and separator of air constituents for a liquid air engine |
| 10/13/1992 | US5154050 Thrust vector control using internal airfoils |
| 10/06/1992 | US5152136 Capable of increased and variable thrust for boost and final, or dash, phases of the mission |
| 09/29/1992 | US5151145 Liner/mandrel for filament wound vessels |
| 09/29/1992 | US5150879 Thruster valve |
| 09/24/1992 | DE4109965A1 Hydrogen ignition system for rocket drive motor - has hydrogen and sulphur di:oxide circulated around annular line |
| 09/22/1992 | US5148674 Method and apparatus for providing real-time control of a gaseous propellant rocket propulsion system |
| 09/08/1992 | US5145355 Apparatus for active monitoring of combustion instability |
| 09/08/1992 | US5144893 Safe ordnance initiation system |
| 09/02/1992 | EP0501038A1 Ignition system for pyrotechnical propulsion device |
| 09/01/1992 | USH1098 Integrated valve assembly |
| 09/01/1992 | US5143328 Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters |
| 08/25/1992 | US5141181 Launch vehicle with interstage propellant manifolding |
| 08/19/1992 | EP0499264A1 Method of producing a catalyst for the decomposition of hydrazine |
| 08/18/1992 | US5138832 Solar thermal propulsion engine |
| 08/13/1992 | DE4103075A1 Sealing system for space rocket booster - has annular springs to apply sealing force |
| 08/13/1992 | CA2036132A1 Conversion of the jet stream |
| 08/06/1992 | DE4103593A1 Pressure ratio regulator e.g. for rocket combustion space - has grating sealed against environmental vacuum for storage of laser-emitted energy in thrust nozzle passage |
| 08/04/1992 | USH1088 Process for installing liner in pressure vessel |
| 08/04/1992 | USH1082 Main-stage solid-propellant rocket motor design |
| 07/28/1992 | US5133183 Gel/solid bipropellant propulsion system with energy management capability |
| 07/23/1992 | DE4035880C1 Rotary valve rotor to convey liq. fuels from tank - passes fuel to reaction chamber via pockets in insert body |
| 07/21/1992 | US5131223 Integrated booster and sustainer engine for a missile |
| 07/14/1992 | US5129604 Lateral thrust assembly for missiles |
| 07/14/1992 | US5129599 Hybrid liquid-vapor propellant feed system for aerospace vehicles |
| 07/14/1992 | US5129326 Controlled venting of combustion gases, exothermic reactive mixture layer encases in shell |
| 07/08/1992 | EP0494008A1 Turbopump with axial throughflow booster |
| 07/08/1992 | EP0494007A1 Single throughflow turbopump with booster |
| 07/08/1992 | EP0494006A1 Turbopump with bleed flow booster pump |
| 07/07/1992 | US5127223 Solid rocket motor propellants with reticulated structures embedded therein and method of manufacture thereof |
| 06/30/1992 | US5126612 Active radial magnetic bearing combined with a back-up bearing |
| 06/30/1992 | US5125793 Turbine blade cooling with endothermic fuel |
| 06/30/1992 | US5125596 Fluid shielded movable strut for missile and rocket thrust vector control |
| 06/30/1992 | US5125318 Inflatable device for excluding sea water from a rocket motor |
| 06/30/1992 | US5125229 Nozzleless propulsion unit of low aspect ratio |
| 06/25/1992 | WO1992010661A1 Thrust nozzle for a rotating body |
| 06/23/1992 | US5123611 System for steering a missile by means of lateral gas jets |
| 06/23/1992 | US5123355 Rocket ignition assembly and means and methods for making and using same |
| 06/17/1992 | DE4114303C1 Recovery of liq. oxygen@ from air surrounding air-borne device e.g. aircraft - includes cooling air compressing, expanding, sepg. oxygen@ for cooling purposes, passing liq. nitrogen@ |
| 06/17/1992 | DE4039910A1 Rohrartige vorrichtung, insbesondere fuer blattspitzenantriebe von helikoptern Tube-like device, in particular for blade tip drives helicopters |
| 06/10/1992 | EP0489712A2 Missile steering arrangement using thrust control |
| 06/09/1992 | US5119627 Embedded pressurization system for hybrid rocket motor |
| 06/09/1992 | US5119626 Combined turborocket and ramjet propulsion unit |
| 06/03/1992 | EP0488858A1 Production method for a combustion chamber wall especially for a racket motor and combustion chamber produced by this method |
| 06/02/1992 | US5117627 Method and device to protect a propulsive catalytic bed from degrading passed through by a fuel |
| 05/26/1992 | US5115710 Load-reducing rocket nozzle operation method |
| 05/20/1992 | EP0486401A1 Device for connecting two bodies possessing different expansion characteristics and method of making same |
| 05/19/1992 | US5113763 Consumable igniter for a solid rocket motor |
| 05/19/1992 | US5113650 Reorienting grain direction of calendered insulation sheet stock perpendicular to gas flow in solid propellant rocket motors |