Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
04/1991
04/02/1991US5004184 System of vehicle guidance by continuous gas jets
04/02/1991US5003772 Propulsion system
03/1991
03/27/1991EP0419338A1 Thermal protection skin, a method and a production installation
03/27/1991EP0419319A1 Combustible igniter for solid propellant rocket motor
03/21/1991WO1991003638A1 Security igniter for propulsor
03/19/1991US4999997 Radial pulse motor igniter-sustain grain
03/12/1991US4999156 Bi-dimensional compression method
03/12/1991US4998410 Hybrid staged combustion-expander topping cycle engine
02/1991
02/27/1991EP0413983A1 Production method for a channeled wall thrust nozzle
02/12/1991US4991798 Apparatus for filling cryogenic engines of a launcher with automatic separation on lift-off
02/12/1991US4991393 Vehicle
02/07/1991DE3924858A1 Ramjet engine with gaseous fuel generators - has bulkhead to protect auxiliary generates from heat of main generators
01/1991
01/30/1991EP0287582B1 A method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage
01/22/1991US4986068 Hypersonic scramjet engine fuel injector
01/18/1991WO1991001478A1 Lateral thrust assembly for missiles
01/18/1991CA2064208A1 Lateral thrust assembly for missiles
01/09/1991EP0407149A1 Precision controlled variable thrust solid propellant rocket motor
01/07/1991CA2018999A1 Precision controlled variable thrust solid propellant rocket motor
01/01/1991US4981033 Mapping the burning of a solid rocket fuel
12/1990
12/27/1990WO1990015960A1 Methods and apparatus for cryogenic removal of solid materials
12/25/1990US4980601 Igniter plug particularly for use in very low temperature liquid fuel
12/25/1990US4979697 Control propulsion unit, especially for exerting transverse forces on a missile
12/20/1990DE3919781A1 Cold gas thrust generation system e.g. for satellite positioning - has concentric control and regulating nozzles and opposed regulating nozzle
12/19/1990EP0403372A1 Combined turbo-stato-rocket jet engine
12/12/1990EP0402268A1 Pyrotechnic igniter for military charges or a reactor or a gas generator
12/12/1990EP0401801A1 Piezoelectric crystal-powered laser ignition device
12/09/1990CA2017495A1 Pyrotechnic igniter for weapon loads or thruster or gas generator
12/04/1990USH853 Cured graphite, epoxy resin structure containing slits
12/04/1990US4974415 Staged, coaxial multiple point fuel injection in a hot gas generator
11/1990
11/28/1990CN1047365A Ring jet engine
11/27/1990US4972673 Solid rocket motor with dual interrupted thrust
11/27/1990CA1276792C Threaded polar openings for composite pressure vessels
11/22/1990EP0398787A1 Tufted thermal protection layer and production method therefor
11/20/1990US4970857 Energy absorber for translating portions of rocket motor cases using honeycomb
11/14/1990EP0396736A1 Sustainer propulsion system
11/13/1990US4969327 Hypersonic scramjet engine fuel injector
11/06/1990US4967599 Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor
11/06/1990CA1275812C Multi-stage rocket motor nozzle throat
10/1990
10/23/1990US4964339 Multiple stage rocket propelled missile system
10/09/1990US4961313 Thermally initiated mechanically fired device for providing protection against slow cook-off
10/04/1990WO1990011438A1 Hot gas generator
09/1990
09/26/1990EP0388613A1 Combined propulsion unit for sub-to hypersonic flight speeds
09/18/1990US4957249 Thrust vector control flap with a merging convex, concave inner contour, for jet aircraft and method for operating the same
09/18/1990US4956971 Solid propellant canister loaded multiple pulsed or staged rocket motor
09/14/1990WO1990010724A1 Pyrotechnic materials
09/14/1990WO1990010611A1 Pyrotechnic materials
09/12/1990EP0257040B1 Low pressure reaction control propulsion system for a spacecraft
09/11/1990US4956201 Method of creating pasageways in niobium by CVD of niobium over sintered vanadium which is thereafter leached
09/11/1990US4955559 Thrust vector control system for aerospace vehicles
09/11/1990US4955558 Reaction control system
09/11/1990US4955202 Hot gas generator
09/05/1990EP0385878A1 Guiding system for a missile making use of continuous gas jets
09/05/1990EP0385004A1 Multiple propellant solid rocket motor
09/04/1990US4953476 Siloxane-based elastomeric interceptor motor insulation
09/03/1990CA2011352A1 Vector guiding system using continuous gas jets
08/1990
08/28/1990US4952254 High impulse, non-detonable propellant
08/28/1990US4951463 Hypersonic scramjet engine fuel injector
08/21/1990US4950341 High-performance propellant combinations for a rocket engine
08/21/1990US4949618 Missile protection system
08/14/1990US4947644 Diverging portion of discontinuous curvature for a rocket engine nozzle
08/09/1990DE3903602A1 Use of magnetic fields in rocket motors
08/08/1990EP0380591A1 Fiber/resin composites, and method of making the same.
07/1990
07/24/1990US4942653 Production method for a channeled wall thrust nozzle
07/03/1990USH795 Reduced temperature sensitivity launch motor
07/03/1990US4938932 Monolithic high activity catalyst bed for a catalytic gas generator
07/03/1990US4938824 Method for making a composite component using a transverse tape
07/03/1990US4938814 High-performance propellant combinations for a rocket engine
07/03/1990US4938021 For a missile
06/1990
06/27/1990EP0375515A1 Dismountable coupling device between two parts subject to high stress
06/27/1990EP0375435A2 Method of developing and making an article having a pre-determined reliability level
06/27/1990EP0374382A1 Cooling for components of hypersonic propulsors
06/26/1990US4936525 Composite rocket motor with integrated composite fins, and method of manufacture
06/26/1990US4936092 Propellant grain design
06/26/1990US4936091 Two stage rocket combustor
06/22/1990CA2004024A1 Method of developing and making an article having a pre-determined reliability level
06/20/1990EP0374020A1 High-pressure turbo pump providing a rocket motor with fuel
06/14/1990CA2005263A1 Releasable connector for interconnecting two parts subjected to high stresses
06/13/1990EP0373128A2 Ignition system
06/13/1990EP0372139A1 Membrane seal for application to pulsed rocket motor
06/06/1990EP0371867A1 Filling device for cryogenic rocket fuel, automatically separated at launching
06/05/1990US4930541 Variable orifice diverter valve
06/05/1990US4930310 Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust
05/1990
05/31/1990DE3839969A1 Elastic spacer ring for a grain arranged in a combustion chamber
05/30/1990EP0370887A1 Rocket nozzle having a divergent skirt with an annular complementary nozzle
05/30/1990EP0258370B1 Reaction jet control system
05/29/1990US4929158 Turbopump with actine suspension for a propulsion system
05/22/1990US4927481 By alternating layers of elastomeric and reinforcement materials
05/21/1990CA2003271A1 Diverter for rocket motor having a complementary annular jet nozzle
05/15/1990US4924775 Integrated two stage rocket
05/03/1990WO1990004714A1 Sustainer propulsion system
04/1990
04/17/1990US4917968 High temperature corrosion resistant composite structure
04/17/1990US4916896 Multiple propulsion with quatro vectorial direction system
04/10/1990US4915883 Method of and apparatus for purging an annular bayonet
04/10/1990US4915754 Reticulated structure embedded in propellant material including a highly plasticized binder
04/04/1990EP0362054A1 Gas injection device for a combined turbo-stato-rocket thruster
04/04/1990EP0362053A1 Combined propulsion system having a structure compatible with two types of operation
04/04/1990EP0362052A1 Nozzle structure for a combined turbo-static rocket
04/03/1990US4913472 Sealed joint for a rocket employing fused inorganic vitreous material
04/03/1990US4912925 For a space craft vehicle
03/1990
03/27/1990US4911795 Method of preserving a composite material cased solid propellant rocket motor
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