| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 07/04/2000 | US6082678 Geostationary earth observation satellite incorporating multiple thruster liquid propellant apogee maneuver system |
| 07/04/2000 | US6082098 Ignition system for rocket engines |
| 07/04/2000 | US6082097 Hybrid rocket system and disposable cartridge for use therein |
| 06/29/2000 | DE19858197A1 Engine, operated with injected propellant, has ceramic bonded or mechanically joined combustion chamber, insulation and nozzle components made of carbon fiber-reinforced silicon carbide |
| 06/28/2000 | EP1013412A1 Integrally woven ceramic composites |
| 06/28/2000 | EP0767872B1 Solid propellant dual phase rocket motor |
| 06/27/2000 | US6079202 Reloadable/modular solid propellant rocket motor |
| 06/27/2000 | US6079101 Rocket engine with one-piece combustion chamber step structure, and its fabrication |
| 06/21/2000 | EP1010885A2 Ignitor for liquid fuel rocket engines |
| 06/15/2000 | WO2000034731A2 Gas generating eject motor |
| 06/15/2000 | WO2000034641A1 Rocket nozzle contour for flow separation control and side load reduction |
| 06/14/2000 | EP1008146A4 Micro gas rheostat |
| 06/14/2000 | EP1008146A1 Micro gas rheostat |
| 06/13/2000 | US6073437 Stable-combustion oxidizer for hybrid rockets |
| 06/08/2000 | WO2000032920A1 Nozzle structure for rocket nozzles having cooled nozzle wall |
| 06/07/2000 | EP1005949A1 Method of forming a rocket thrust chamber |
| 06/07/2000 | EP1005948A1 Method of forming a rocket thrust chamber |
| 05/31/2000 | EP1003989A1 Quick-acting valve |
| 05/30/2000 | US6068010 Microvalve and microthruster for satellites and methods of making and using the same |
| 05/16/2000 | US6063219 Higher density inhibited red fuming nitric acid (IRFNA) oxidizer gel |
| 05/16/2000 | US6062018 Pulse detonation electrical power generation apparatus with water injection |
| 05/16/2000 | CA2048641C Pyrotechnic materials |
| 05/09/2000 | US6058697 Hybrid rocket system and integrated motor for use therein |
| 05/04/2000 | WO2000024693A2 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 05/04/2000 | CA2342366A1 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 05/02/2000 | US6055871 Machine for cutting a cylindrical specimen of rocket propellant |
| 04/25/2000 | US6054521 Erosion resistant-low signature liner for solid propellant rocket motors |
| 04/25/2000 | US6052987 Non-propellant fluid cooled space craft rocket engine |
| 04/20/2000 | WO2000022291A2 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 04/20/2000 | WO2000005133A3 High regression rate hybrid rocket propellants |
| 04/18/2000 | US6050085 Method of injecting a first and a second fuel component and injection head for a rocket |
| 04/13/2000 | WO2000020749A1 Method for manufacturing outlet nozzles for rocket engines |
| 04/11/2000 | US6047541 HAN TEAN (xm-46) mixing gas generator propellant tank pressurizer for launch vehicles and spacecraft |
| 04/04/2000 | US6045638 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 03/29/2000 | EP0988456A2 Assembly including tubular bodies mated with a compression loaded adhesive bond |
| 03/29/2000 | EP0988446A1 Device for anchoring a member activating an adjustable nozzle |
| 03/29/2000 | EP0960317A4 Case for combustible materials and methods for making and using the same |
| 03/28/2000 | US6042671 Members for rocket nozzle formed by stacking adhesives with several layers between nozzle extension part heat-resistant element and composite structural body |
| 03/23/2000 | WO1999065769A3 Electrical drive system for rocket engine propellant pumps |
| 03/16/2000 | WO2000014397A2 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
| 03/14/2000 | US6035631 Safety in solid fuel rocket motors |
| 03/07/2000 | US6032904 Multiple usage thruster mounting configuration |
| 03/07/2000 | US6032545 Nozzle flow thrust vector measurement |
| 03/02/2000 | WO2000011338A1 Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the same |
| 02/29/2000 | CA2176048C Missile jet vane control system and method |
| 02/23/2000 | CN1245480A Method and apparatus for total energy fuel conversion systems |
| 02/22/2000 | US6026749 Multiple base propellant with combustion inhibitor |
| 02/17/2000 | WO1999061773A3 Anti-slosh liquid propellant tank for launch vehicles |
| 02/17/2000 | DE19937812A1 Composite heat exchanger, which uses materials that enable it to operate at high elevated temperatures, such as for in a nuclear fusion reactor |
| 02/15/2000 | US6024810 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 02/15/2000 | US6024328 Satellite control method using single species of bipropellant |
| 02/15/2000 | US6023983 Machine for excising a specimen of rocket propellant |
| 02/10/2000 | WO2000006883A1 Method for increasing the specific impulse in a liquid-propellant rocket engine and rocket power unit for realising the same |
| 02/10/2000 | DE19813949A1 Aircraft jet engine uses an additional injection of water under high pressure into the combustion zone with the fuel/air mixture for increased thrust and with laser spark plugs for continuous combustion |
| 02/03/2000 | WO2000005133A2 High regression rate hybrid rocket propellants |
| 02/03/2000 | CA2338213A1 High regression rate hybrid rocket propellants |
| 02/02/2000 | EP0975863A2 Missile with safe rocket ignition system |
| 01/25/2000 | US6016652 Hybrid rocket system with disposable cartridge |
| 01/18/2000 | US6014857 High fuel regression hybrid rocket motor |
| 01/13/2000 | DE19828199A1 Absperrventil Shut-off valve |
| 01/06/2000 | WO2000000731A1 Compact and adjustable tailpipe for piloting aerospace craft |
| 12/29/1999 | EP0809783B1 Fire mitigation device |
| 12/23/1999 | WO1999065769A2 Electrical drive system for rocket engine propellant pumps |
| 12/22/1999 | EP0784781B1 Solid fuel launch vehicle destruction system and method |
| 12/21/1999 | US6003301 Exhaust nozzle for multi-tube detonative engines |
| 12/15/1999 | EP0963515A1 Acoustic igniter and ignition method for propellant liquid rocket engine |
| 12/15/1999 | EP0828929A4 Reduced pollution power generation system and gas generator therefore |
| 12/02/1999 | WO1999061774A1 Modular solid-fuel rocket propelling charges with a casing, a fill-drain system, cooling and suspension |
| 12/02/1999 | WO1999061773A2 Anti-slosh liquid propellant tank for launch vehicles |
| 12/02/1999 | WO1999061238A1 Non-asbestos insulation for rocket motor casing |
| 12/02/1999 | CA2328083A1 Non-asbestos insulation for rocket motor casing |
| 12/01/1999 | EP0960317A2 Case for combustible materials and methods for making and using the same |
| 11/18/1999 | WO1999058233A1 Liquid spray nozzle and use of same |
| 11/17/1999 | EP0956441A1 Unfolding injector tube for propulsion unit |
| 11/16/1999 | US5985361 Polymeric binder with hydroxyl groups; isocyanate curing agent; cohesive strength; stoichiometry insensitive |
| 11/16/1999 | US5984369 Assembly including tubular bodies and mated with a compression loaded adhesive bond |
| 11/16/1999 | US5983626 Injection head for rocket engines |
| 11/11/1999 | WO1999032780B1 Missile with safe rocket ignition system |
| 11/10/1999 | CN1234316A Method for producing high heat-flux regenerative loop for rocket engine combustion chamber |
| 11/04/1999 | DE19817818A1 Flat drive for aircraft and space rockets |
| 11/03/1999 | EP0953759A2 Injector and ignition system for rocket engines |
| 11/02/1999 | US5976293 Method for making a case for combustible materials |
| 10/26/1999 | US5970705 Variable configuration final nozzle assembly for a combined rocket/ramjet engine |
| 10/26/1999 | US5970702 Reduced pollution hydrocarbon combustion gas generator |
| 10/21/1999 | WO1999053185A1 Device for anchoring a member activating an adjustable nozzle |
| 10/13/1999 | EP0809755B1 Thrust chambers |
| 10/07/1999 | WO1999032780A3 Missile with safe rocket ignition system |
| 10/05/1999 | US5961074 Method and apparatus for pressurized feeding of liquid propellants to a rocket engine |
| 09/30/1999 | WO1999049186A1 Heat shielding structure |
| 09/30/1999 | DE19813330A1 Lateral thrust generating process for use with projectiles, e.g. satellites, guided missiles etc. |
| 09/29/1999 | EP0945596A1 Thermal protection structure |
| 09/29/1999 | EP0898497A4 Electroformed multilayer flow regulator |
| 09/28/1999 | US5959235 Fire mitigation device |
| 09/28/1999 | US5956937 Reduced pollution power generation system having multiple turbines and reheater |
| 09/22/1999 | EP0943795A1 Production method for a regenerative heat exchange circuit for high thermal flow, especially for rocket combustion chambers |
| 09/16/1999 | WO1999046499A1 Rifled jet nozzle |
| 09/15/1999 | EP0941925A2 Propellant tank |
| 09/08/1999 | CN1227913A Method of and apparatus for manufacturing solid rocket motors |
| 09/01/1999 | EP0939216A1 Integrated propulsion plant with at least a ramjet and a scramjet operational mode |
| 08/26/1999 | WO1999042706A1 Electricity generation system for use with cryogenic liquid fuels |