Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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08/25/1999 | EP0937644A2 Space craft axis stabilizer apparatus, system and method |
08/25/1999 | CN1226484A Electric vehicle with battery regeneration dependent on battery charge state |
08/24/1999 | US5941062 Pulse rocket engine |
08/19/1999 | DE19804232A1 Combustion chamber for motors and high power tuyeres |
08/17/1999 | US5938975 Method and apparatus for total energy fuel conversion systems |
08/10/1999 | US5936737 Wheelset sensing system |
08/10/1999 | US5936188 Missile with a safe rocket ignition system |
08/04/1999 | EP0932807A1 Design for a gun-launched rocket |
08/03/1999 | US5932940 Microturbomachinery |
08/03/1999 | US5931414 Missile for combatting moving targets |
07/28/1999 | EP0931851A1 Method for obtaining functional metallic, ceramic or ceramic/metallic layers on the internal wall of hollow bodies |
07/27/1999 | US5928545 Cure shrinkage measurement |
07/27/1999 | US5927335 For inclusion within a pressure vessel of a gas generator |
07/27/1999 | CA2048642C Pyrotechnic materials |
07/21/1999 | EP0670776B1 High thermal conductivity non-metallic honeycomb |
07/13/1999 | US5921167 Hermetic shear seal for piston displacement fuel tank |
07/08/1999 | WO1999034105A1 Acoustic igniter and ignition method for propellant liquid rocket engine |
07/07/1999 | EP0927299A1 Combustion chamber and method for producing a combustion chamber |
07/06/1999 | US5918460 Liquid oxygen gasifying system for rocket engines |
07/01/1999 | WO1999032780A2 Missile with safe rocket ignition system |
06/23/1999 | EP0924424A2 Liquid tripropellant rocket engine coaxial injector |
06/23/1999 | EP0924423A2 Method of manufacturing solid fuel rocket motors |
06/22/1999 | US5913678 Arrangement for sealing combustion-chamber bricks |
06/17/1999 | DE19810638C1 Oxidiser-fuel tank for space vehicle vectoring motor |
06/09/1999 | EP0921024A2 Electric vehicle with battery regeneration dependant on battery charge state |
06/09/1999 | EP0920575A1 Microturbomachinery |
06/09/1999 | CN1219141A Electroformed multilayer flow regulator |
06/02/1999 | EP0919464A1 Spacecraft attitude and velocity control thruster system |
05/19/1999 | EP0916835A1 Closed loop cooled rocket engine |
05/18/1999 | US5903976 Method of manufacturing a combustion enclosure with cooling by transpiration |
05/14/1999 | WO1999022903A1 A method for producing rotational-symmetrical articles of sheet metal with double curved surface and varying thickness of material |
05/11/1999 | US5901550 Liquid fueled pulse detonation engine with controller and inlet and exit valves |
05/04/1999 | US5899388 For a combustion member |
05/04/1999 | US5899060 Wall structure for fuel-cooled rocket engine walls |
04/28/1999 | EP0910494A2 Method for making a rhenium rocket nozzle |
04/20/1999 | US5894723 Rocket engine nozzle with ejectable inserts |
04/15/1999 | WO1998058179A3 Assembly including tubular bodies mated with a compression loaded adhesive bond |
04/13/1999 | US5893266 Hybrid rocket system and integrated motor for use therein |
03/31/1999 | EP0737271B1 Discus-shaped aerodynamic vehicle for use at extremely high velocities |
03/30/1999 | US5887821 Mechanism for thrust vector control using multiple nozzles and only two yoke plates |
03/24/1999 | EP0903487A2 Integrated pulsed propulsion system for microsatellite |
03/24/1999 | EP0871582A4 Apparatus and method for controlling the motion of a solid body or fluid stream |
03/24/1999 | EP0804362A4 Satellite fueling system and method therefor |
03/23/1999 | US5886289 Long range artillery shell |
03/09/1999 | US5880356 Device for pressurizing a unified two-liquid propulsion subsystem geostationary satellites |
03/03/1999 | EP0899534A2 Variable thrust nozzle system |
03/03/1999 | EP0899449A2 Rocket engine having a transition attachment between a combustion chamber and an injector |
03/03/1999 | EP0899448A2 Fabrication of a rocket engine with transition structure between the combustion chamber and the injector |
03/03/1999 | EP0899447A2 Attachment ring for a rocket combustion chamber |
03/03/1999 | EP0898497A1 Electroformed multilayer flow regulator |
02/24/1999 | EP0897863A2 Filter assemblies and vehicles incorporating filter elements |
02/24/1999 | CN1209189A 火箭发动机喷管 Rocket engine nozzle |
02/23/1999 | US5874015 Method for making a rhenium rocket nozzle |
02/23/1999 | US5873241 Rocket engine auxiliary power system |
02/23/1999 | US5873240 Pulsed detonation rocket engine |
02/18/1999 | WO1999008030A1 Quick-acting valve |
02/18/1999 | WO1998046960A3 Adhesive bonded case assembly for rockets |
02/02/1999 | US5865207 Rocket fuel lines |
02/02/1999 | US5865030 Gas turbine combustor with liquid fuel wall cooling |
01/28/1999 | WO1999004156A1 Combustion chamber and method for producing a combustion chamber |
01/27/1999 | EP0893344A1 Compact monolithic propulsion system using monergol for small satellite |
01/26/1999 | US5862670 Cyrogenic upper stage for reusable launch vehicle |
01/21/1999 | DE19730674A1 Brennkammer und Verfahren zur Herstellung einer Brennkammer Combustion chamber and method of manufacturing a combustion chamber |
01/12/1999 | US5857323 Rocket engine burner with porous metal injector for throttling over a large thrust range |
01/05/1999 | US5855828 Method of forming a composite structure such as a rocket combustion chamber |
01/05/1999 | US5855827 Pulse detonation synthesis |
12/30/1998 | EP0620895B1 Satellite propulsion and power system |
12/24/1998 | DE19822845A1 Modular solid rocket propellant charges |
12/23/1998 | WO1998058179A2 Assembly including tubular bodies mated with a compression loaded adhesive bond |
12/23/1998 | CN1202952A Controlled temperature rocket nozzle |
12/23/1998 | CA2297785A1 Assembly including tubular bodies mated with a compression loaded adhesive bond |
12/22/1998 | US5850989 Method and system for rapidly assembling a launch vehicle |
12/10/1998 | WO1998036975A3 Case for combustible materials and methods for making and using the same |
12/03/1998 | WO1998054464A2 Jet engine |
12/02/1998 | EP0880645A1 Rocket engine nozzle |
11/25/1998 | CN1199658A Producing method for cavity substance |
11/24/1998 | US5840227 Method of making internal thermal protection for a thruster |
11/24/1998 | US5839272 Dual concentric poppet valves for maintaining substantially constant the ratio of two fluid flows over an operating range of valve opening |
11/18/1998 | EP0810946B1 Device for pressurising a unified two-liquid propulsion subsystem for geostationary satellites |
11/17/1998 | US5836543 Discus-shaped aerodyne vehicle for extremely high velocities |
11/17/1998 | US5836542 Flying craft and a thruster engine suitable for use in such a craft |
11/17/1998 | US5836150 Micro thrust and heat generator |
11/12/1998 | WO1998050694A1 Spherical chamber fluidic ball diverter valve |
11/12/1998 | DE19734845C1 Rapid-action valve for space vehicle steering circuits |
11/10/1998 | US5832719 Rocket thrust chamber |
10/27/1998 | US5827993 Pyrotechnic ignition device for a gas generator |
10/22/1998 | WO1998046960A2 Adhesive bonded case assembly for rockets |
10/21/1998 | EP0871582A2 Apparatus and method for controlling the motion of a solid body or fluid stream |
10/20/1998 | US5823478 For a rocket engine |
10/19/1998 | CA2235113A1 Process for the production of an object with a hollow space |
10/14/1998 | EP0870105A1 Extendable divergent tail pipe for propulsion unit |
10/13/1998 | US5821284 Includes ammonium sulfate and antimony oxide, which when combined have a synergistic effect that reduces the ablation rate significantly; also includes epdm rubber and aramid fibers |
10/13/1998 | US5820100 Electromagnetic linear actuator with movable plates and valve fluid regulator controlled by the actuator |
10/13/1998 | US5819526 Low power arcjet propellant feed system |
10/06/1998 | US5817968 Gas generation with high pressure sensitivity exponent propellant |
10/06/1998 | US5816539 Orbital assist module and interstage |
09/15/1998 | US5808231 Solid propellant combustion apparatus |
09/15/1998 | US5806791 Missile jet vane control system and method |
09/09/1998 | EP0862688A1 Controlled temperature rocket nozzle |
09/08/1998 | US5802842 For use in a rocket engine |