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)
09/1997
09/02/1997US5661970 Thrust-generating device
08/1997
08/27/1997EP0791742A1 Low power arcjet propellant feed system
08/27/1997EP0791741A1 Thermal insulation for solid rocket motor
08/26/1997US5660039 Injection system and an associated tricoaxial element
08/19/1997US5657948 Control of a projectile by multi-chamber and single-nozzle impeller
08/14/1997WO1997029277A1 Rocket engine nozzle
08/13/1997EP0767872A4 Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture
07/1997
07/29/1997US5652052 Bi-composite joint using continuous fiber
07/23/1997EP0784781A1 Solid fuel launch vehicle destruction system and method
07/17/1997WO1997025623A2 Controlling motions of a solid body or fluid stream
07/15/1997US5647201 Cavitating venturi for low reynolds number flows
07/10/1997WO1997024521A1 Extendable divergent tail pipe for propulsion unit
07/10/1997DE19602731C1 Reduced thermal stress wall structure for a rocket drive mechanism
07/08/1997US5645219 Addition-polymerization resin systems for fiber-reinforced nozzle ablative components
07/08/1997US5645127 Coolant supply arrangement for jet engine turbine walls
07/08/1997US5644920 In a vehicle liquid propellant tank
07/02/1997EP0679134B1 Radial four-blade thrust vector
06/1997
06/25/1997EP0780564A2 High temperature thrust chamber for spacecraft
06/25/1997EP0780563A2 Rocket thrust chamber
06/24/1997US5641123 Expandable nozzle mechanism for a rocket engine
06/24/1997US5640844 For delivering a liquid fuel component to a rocket engine
06/19/1997DE19650411A1 Maximising hybrid rocket fuel regression rate
06/19/1997DE19601507C1 Flame blow back tester for engine component groups
06/17/1997US5638683 Injection device
06/11/1997EP0778200A2 Multi-stage space transport system and method for horizontal-takeoff
06/10/1997US5636513 For the operation of a near unity blowdown reactor
06/05/1997DE19545711C1 Reusable carrier body as starting aid for flight craft
06/03/1997US5635665 Linear gas generant and filter structure for gas generator
05/1997
05/21/1997EP0773883A1 Two stage launch vehicle and launch trajectory method
05/20/1997US5630564 Differential yoke-aerofin thrust vector control system
05/06/1997US5626313 Engine assembly including fuel storage bladder
04/1997
04/22/1997US5622611 Electroformed multilayer flow regulator incorporating force-generating means for selectively constricting the fluid flow path, and a process for the preparation thereof
04/22/1997US5622046 Multiple impinging stream vortex injector
04/17/1997WO1997014160A1 Electromagnetic linear actuator having movable plates and a fluid flow controller with valves controlled by said actuator
04/16/1997EP0767872A1 Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture
04/15/1997US5619851 Rocket nozzle for a rocket engine
04/01/1997US5616884 Propellant gas-generation system for canister ejection
04/01/1997US5615983 Propellant grain machining device and method
03/1997
03/27/1997DE19632801A1 Compression of intensely-cooled liquid fuel for rockets, etc.
03/25/1997US5613358 Reduced cost membrane seal assembly for pulsed rocket motor
03/25/1997US5613299 Method of fabricating a rocket thrust chamber
03/19/1997EP0763468A1 Economic launch vehicle
03/06/1997WO1997008442A1 Rocket engine burner with porous metal injector
03/04/1997US5607123 For positioning a rocket nozzle
02/1997
02/27/1997WO1997007331A1 Shape of combustion chamber of solid fuel rocket
02/19/1997EP0758283A1 Fabrication of tubular wall thrust chambers for rocket engines using laser powder injection
02/18/1997US5603213 Injection system with concentric slits and the associated injection elements
02/11/1997US5600946 Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture
02/06/1997WO1997004231A1 Method and apparatus for pressurized feeding of liquid propellants to a rocket engine
02/05/1997EP0757184A2 Cavitating venturi for low reynolds number flows
02/04/1997US5598762 Fluid storage tank employing an isolation seal
02/04/1997US5598699 Laser initiated non-linear fuel droplet ignition apparatus
01/1997
01/23/1997WO1997002464A1 Improved safety in solid fuel rocket motors
01/23/1997DE19540514C1 Power-plant, esp. for space vehicles and using liquid propellant
01/23/1997DE19540378C1 Release device for rocket pipes, especially for aggressive propellants
01/21/1997US5596166 Penetrating vehicle with rocket motor
01/02/1997DE19523013A1 Hydrazine-fuelled rocket for space travel
12/1996
12/27/1996WO1996041940A1 Supersonic jet with a controllable critical cross section
12/19/1996DE19521543A1 Thruster jet using monopropellant e.g. hydrazine
12/10/1996US5582366 Satellite fueling system and method therefor
12/10/1996US5582001 Hybrid rocket combustion enhancement
12/10/1996US5582000 Coolable rocket nozzle for a rocket engine
12/03/1996US5579636 Pyrotechnic valve, igniter and combustion preheater for hybrid rocket motors
12/03/1996US5579635 Distributed erosion region rocket motor nozzle
12/03/1996US5579576 Reaction motor structure and method of construction
11/1996
11/27/1996EP0744591A2 Missile jet vane control system and method
11/14/1996DE19618740A1 Rocket drive using liquid fuels
11/12/1996US5572865 Satellite propulsion and power system
11/12/1996US5572864 Solid-fuel, liquid oxidizer hybrid rocket turbopump auxiliary engine
11/05/1996US5570573 Combustion chamber for a thruster with a sealed connection between an end wall and a composite tubular structure
10/1996
10/31/1996WO1996033803A1 Carbides and nitrides of transition elements applied on the catalytic decomposition of hydrazine
10/31/1996DE19616838A1 Flammable chamber with evaporation cooling
10/31/1996CA2219149A1 Carbides and nitrides of transition elements applied on the catalytic decomposition of hydrazine
10/30/1996EP0740063A1 Injector of coaxial configuration for a rocket combustion chamber
10/29/1996US5568901 Two stage launch vehicle and launch trajectory method
10/29/1996US5568723 For an electrothermal thruster
10/25/1996CA2101175A1 Propellant gas-generation system for canister ejection
10/23/1996EP0602031B1 The initiation of propellants
10/22/1996US5566544 In a rocket engine
10/22/1996CA2001315C Reverse bulged forward acting scored rupture disc bulkhead structure for multi-staged rocket motor
10/16/1996EP0737271A1 Discus-shaped aerodynamic vehicle for use at extremely high velocities
10/15/1996US5564272 Slotted hybrid pressure vessel
10/09/1996EP0735991A1 Process for operating a reaction-type missile propulsion system and missile propulsion system
10/01/1996US5560559 Thrust-vectoring apparatus
09/1996
09/24/1996US5557928 Tube rocket thrust chamber construction and method
09/24/1996US5557927 Blanching resistant coating for copper alloy rocket engine main chamber lining
09/18/1996EP0732494A2 Cooling the walls of rockets or jet engines
09/10/1996US5554818 Lithium water reactor
09/03/1996US5551230 Heat induced high pressure lox pump rocket engine cycle
08/1996
08/29/1996WO1996026108A1 Device for pressurising a unified two-liquid propulsion subsystem for geostationary satellites
08/22/1996WO1996025643A1 Fire mitigation device
08/22/1996WO1996025595A1 Thrust chambers
08/21/1996EP0727403A1 Inverse hybrid propulsion system
08/20/1996US5546656 Fabrication of rocket thrust chambers
08/07/1996EP0725259A1 Projectile control by a multi-chamber, single nozzle thruster
08/07/1996EP0725253A2 Gas turbine combustor
08/07/1996EP0724485A1 Propellant grain cutting assembly
07/1996
07/30/1996US5541413 Acousto-optic tunable filter-based surface scanning system and process
07/25/1996WO1996022222A1 Satellite fueling system and method therefor
07/11/1996WO1996020867A1 Fluidic control thrust vectoring nozzle
1 ... 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 ... 47