| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 06/28/1994 | US5323953 Pressurised storage for gases |
| 06/23/1994 | DE4242977A1 Container with flexible outer walls for holding fluid material |
| 06/22/1994 | EP0602668A1 Propellant immobilizing method |
| 06/22/1994 | EP0602031A1 The initiation of propellants. |
| 06/16/1994 | DE4341376A1 Rocket motor for liq. propellant - has injection unit with injection plate, and nozzles for propellant in high and low mixture ratios |
| 06/15/1994 | EP0601305A1 Rocket based on catalytic and for thermal decomposition |
| 06/14/1994 | US5319926 Thruster for spacecraft |
| 06/09/1994 | WO1994012865A1 Surface inspection and characterization system and process |
| 06/09/1994 | CA2150108A1 Surface inspection and characterization system and process |
| 06/07/1994 | CA1329992C Hypersonic scramjet engine fuel injector |
| 06/01/1994 | DE4301614C1 Liq. propellant-fuelled missile storage - involves propellant modification to form electro-rheological fluid or liq. crystalline phase |
| 05/26/1994 | DE4305154C1 Coaxial fuel injectors for combustion chamber in rocket - has central body and sleeve, opening in plane of combustion chamber end face, and flow divider |
| 05/24/1994 | US5313789 Solid fuel turbine power plant and method |
| 05/19/1994 | DE4238633A1 Radial displacement control for jet missile - uses 4 steel rudders rotatable about common axis and axially adjustable |
| 05/17/1994 | US5311820 Method and apparatus for providing an insensitive munition |
| 05/10/1994 | US5310159 Destructible core for undercut casting |
| 05/10/1994 | US5309712 Solid fuel rocket motor seals |
| 05/03/1994 | US5307636 Staged, coaxial, multiple point fuel injection in a hot gas generator having a sufficiently wide cone angle |
| 04/28/1994 | DE4301041C1 Providing a fluid cooled tubular wall wiht a thermal protection coating - by coating the wall at its heated work temperature |
| 04/27/1994 | EP0442899B1 Vane-type thrust vectoring nozzle |
| 04/26/1994 | US5305601 Solid fuel rocket motor assembly, and method of making the same |
| 04/14/1994 | WO1994008131A1 Laser initiated non-linear fuel droplet ignition |
| 04/06/1994 | EP0428627B1 Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor |
| 03/24/1994 | DE4304559C1 Cooled structure production method - forms tube wall of small pipes with covering layer thicker at mounting flange and spark-erodes openings in pipes for coolant at flange seat |
| 03/23/1994 | EP0587900A1 Linear gas generating agent and filter construction for gas generator |
| 03/17/1994 | DE4230658A1 Explosive fuelled thrust jet drive in combustion chambers - has exothermal reaction and pressure wave on gas pressure fastening tube and fuel supply |
| 03/16/1994 | EP0587126A1 Long life catalytic gas generator for space propulsion applications |
| 03/08/1994 | CA1327454C Multiple propellant solid rocket motor |
| 03/03/1994 | WO1994004420A1 Fluid dispensing unit with metered outflow |
| 02/24/1994 | DE4227907A1 Liquid-fuelled rocket injection system - has rotary casing with ports slid pneumatically or hydraulically so as to vary free cross-section of injection ports |
| 02/22/1994 | US5288537 Connected cells from fibers impregnated with matrix resin, for controlling direction of heat transfer |
| 02/16/1994 | EP0583176A1 Self-propelled stabilised infrared decoy |
| 02/09/1994 | EP0582427A1 Reducing thermal deposits in propulsion systems |
| 02/08/1994 | US5284309 Propellant immobilizing system and method |
| 02/01/1994 | US5282576 Self-locking and reversible mechanism for deploying the diverging portion of a rocket engine nozzle |
| 02/01/1994 | US5282357 High-performance dual-mode integral propulsion system |
| 02/01/1994 | US5282356 Flywheel engine |
| 01/26/1994 | EP0579919A1 Pneumatic linear drive with locking for ends of travel |
| 01/25/1994 | US5280706 Composite/metal hybrid rocket motor case and methods for manufacturing |
| 01/18/1994 | US5279484 Manned space vehicle with low-level hydrogen-oxygen-carbon dioxide propulsion unit |
| 01/18/1994 | US5279447 Fluid dispensing unit with metered outflow |
| 01/18/1994 | CA1326127C Filament winding of case onto solid propellant grain |
| 01/11/1994 | US5277863 Method of preparing non-composite, thermoplastic, high-temperature-resistant rocket motor cases |
| 01/04/1994 | US5275000 Reducing thermal deposits in endothermic fuel reactors of propulsion systems |
| 01/04/1994 | US5274998 Disposal of solid rocket fuel by burning in rocket motor chamber; injecting neutralizing fluid; salt formation with chlorine |
| 12/28/1993 | US5273785 Methods and compositions for bonding propellants within rocket motors |
| 12/28/1993 | US5273603 Filament winding using different size mandrels and angles |
| 12/21/1993 | US5271226 High speed, amplitude variable thrust control |
| 12/07/1993 | US5267841 Peristaltic injector |
| 12/07/1993 | US5267437 Dual mode rocket engine |
| 12/02/1993 | DE4217051A1 Spacecraft rocket fuel system - has parallel ingredient tanks followed by common one forming fuel surface retaining incoming propellant gas |
| 12/02/1993 | DE4216955A1 Liquid-fuelled catalytic propulsion unit - has radial outlet slots inclined to each other in injection-pipe end towards dissolution chamber |
| 11/30/1993 | US5265415 Liquid fuel injection elements for rocket engines |
| 11/24/1993 | EP0571254A1 Transpiration cooled combustion chamber |
| 11/23/1993 | US5263666 Spacecraft with increased stationkeeping fuel load |
| 11/11/1993 | WO1993022655A1 Acousto-optic tunable filter-based surface scanning system and process |
| 11/11/1993 | CA2133307A1 Acousto-optic tunable filter-based surface scanning system and process |
| 10/19/1993 | US5253584 Oxidizing halogenated polymer and layer of oxidizable metal,or alloy therof,reacting exothermically on ignition |
| 10/19/1993 | CA1323352C Low pressure reaction control propulsion system for a spacecraft |
| 10/12/1993 | US5251852 Thermal fuel transfer and tank isolation to reduce unusable fuel |
| 10/12/1993 | US5251436 Thrust-reducing, chaotic-flow nozzle |
| 10/05/1993 | USH1234 Solid propellant air-turborocket |
| 10/05/1993 | US5249357 Method of fabricating a rocket engine combustion chamber |
| 09/30/1993 | WO1993018910A1 High thermal conductivity non-metallic honeycomb |
| 09/28/1993 | US5247792 Reducing thermal deposits in propulsion systems |
| 09/28/1993 | CA1322548C Thrust vector control system for aerospace vehicles |
| 09/22/1993 | EP0561537A1 Segmented structure for rocket motors |
| 09/08/1993 | EP0559436A1 Solid propellant rocket motor case, comprising a material which melts down at undesirable temperatures above normal storage temperatures |
| 08/31/1993 | US5240038 Surface tension tank with multiple delivery rates |
| 08/19/1993 | WO1993016019A1 Linear gas generating agent and filter construction for gas generator |
| 08/17/1993 | US5236529 Fringed thermal protection device and method of manufacturing it |
| 08/12/1993 | DE4203775A1 Hydrazine fuelled propulsion unit with decomposition chamber - has injection bores inclined to lines perpendicular to one or more injector head outer surfaces |
| 08/10/1993 | US5233755 Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber obtained by the method |
| 08/03/1993 | US5232534 Thermal protection coating, and method and installation for manufacturing it |
| 08/03/1993 | US5232334 Rotary machine having an axial abutment that retracts automatically by means of a flexible membrane subjected to the pressure of a fluid |
| 08/03/1993 | US5232333 Single flow turbopump with integrated boosting |
| 07/28/1993 | EP0552676A1 Protection system for parts subjected to high thermal loads or the thermal loads and dynamic pressure loads |
| 07/28/1993 | CN1074730A Model rocket engine mfg method |
| 07/20/1993 | US5228285 Solid propellant rocket motor case for insensitive munitions requirements |
| 07/13/1993 | US5227208 Integrally wound joint structure |
| 07/13/1993 | US5226598 Nozzle wall |
| 07/06/1993 | US5224817 Shunt flow turbopump with integrated boosting |
| 07/06/1993 | US5224343 Constant fuel supply device for a thruster |
| 06/30/1993 | EP0549402A1 System for damping high frequency combustion instabilities in a combustion chamber |
| 06/30/1993 | CN1021470C Propellant of rocket-engine plants |
| 06/29/1993 | US5222873 Fluid-driven reciprocating apparatus and valving for controlling same |
| 06/29/1993 | US5222361 Rocketjet engine |
| 06/22/1993 | US5221045 Bulge formed cooling channels with a variable lead helix on a hollow body of revolution |
| 06/22/1993 | US5220783 Foamed in place igniter and aft-end assembly for rocket motor comprising the same |
| 06/16/1993 | EP0381753B1 A thermally initiated mechanically fired device for providing protection against slow cook-off |
| 06/08/1993 | US5217188 Modular solid-propellant launch vehicle and related launch facility |
| 06/03/1993 | DE4137638A1 Component with heat protected wall with cooling channels - has heat conductive layer on surface of cooling channel adjoining wall having matching layer and wall thicknesses |
| 05/25/1993 | US5212946 Reloadable/modular solid propellant rocket motor |
| 05/25/1993 | US5212944 Carbon and silicone polymer ablative liner material |
| 05/19/1993 | EP0542606A1 Hydraulicly blocked commanding device for auxiliary jets |
| 05/19/1993 | EP0541917A2 Method of making oxidation resistant CFC-based articles, preferably for space-flights |
| 05/13/1993 | WO1993009339A1 Turbine engine control system |
| 05/11/1993 | US5209876 Cloth-lined interceptor motor insulation for strong insulation-to-propellant interlock |
| 05/04/1993 | US5207399 Vapor pressurization system for outer space |
| 05/04/1993 | US5206989 Method of making solid propellant canister loaded rocket motor |