Patents for F03H 1 - Use of plasma to produce a reactive propulsive thrust (1,048) |
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09/24/1996 | US5559391 Three-grid ion-optical system |
09/03/1996 | US5551904 Method for making an ion thruster grid |
08/28/1996 | EP0662195B1 Reduced length plasma engine with closed electron deviation |
08/27/1996 | US5548953 Stable, lightweight |
07/30/1996 | US5540046 Method and apparatus for pressure pulse arcjet starting |
05/28/1996 | US5519991 Increased efficiency arcjet thruster |
04/30/1996 | US5513087 Power supply |
04/23/1996 | US5509266 Device for measuring variations in the thrust of a plasma acceleration with closed electron drift |
02/29/1996 | WO1996006518A1 Plasma accelerator with closed electron drift |
01/23/1996 | US5485721 Arcjet for a space flying body |
12/13/1995 | CN1030514C Spacecraft with modulated thrust electrostatic ion thruster and associated method |
12/12/1995 | US5475354 Plasma accelerator of short length with closed electron drift |
11/07/1995 | US5465023 Carbon-carbon grid for ion engines |
09/12/1995 | US5448883 Ion thruster with ion optics having carbon-carbon composite elements |
08/30/1995 | EP0669461A1 Three grid ion-optical device |
08/22/1995 | US5444258 Ion-optics system for a source of ions to be discharged into a gas |
08/08/1995 | US5439191 Railgun thruster |
07/19/1995 | EP0519038B1 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure, and a satellite, for implementing same |
07/18/1995 | US5434469 Plasma generation, ion extraction and acceleration in glass chamber |
07/13/1995 | WO1995019038A1 Method and apparatus for generating ions |
07/12/1995 | EP0662195A1 Reduced length plasma engine with closed electron deviation. |
06/20/1995 | US5425231 Gas fed pulsed electric thruster |
06/07/1995 | EP0656170A1 Device for measuring changes in the thrust of a plasma engine with closed electron drift |
05/30/1995 | US5420437 Method and apparatus for generation and implantation of ions |
05/09/1995 | US5414238 Resonant power supply for an arcjet thruster |
05/03/1995 | EP0650557A1 Fixed plasma motor. |
03/30/1995 | DE4321725A1 Engine for spacecraft (space vehicles) |
02/08/1995 | EP0637689A2 Heat-conducting coating for ceramic materials of ion engines |
01/18/1995 | EP0634575A2 Device for distributing a gaseous component in ionization chambers, for space thrusters |
01/18/1995 | EP0581765A4 Long life arcjet thruster having diffuse cathode arc attachment. |
01/05/1995 | WO1995001085A1 Device for measuring changes in the thrust of a plasma engine with closed electron drift |
01/05/1995 | WO1995000758A1 Reduced length plasma engine with closed electron deviation |
01/05/1995 | CA2142607A1 A plasma accelerator of short length with closed electron drift |
01/05/1995 | CA2141605A1 Device for measuring changes in the thrust of a plasma engine with closed electron drift |
12/06/1994 | US5369953 Three-grid accelerator system for an ion propulsion engine |
10/25/1994 | US5359258 Plasma accelerator with closed electron drift |
10/25/1994 | US5359180 Power supply system for arcjet thrusters |
10/25/1994 | US5357747 Pulsed mode cathode |
10/20/1994 | DE4310822A1 Arc-jet engine |
10/20/1994 | DE4310821A1 Arc-jet engine |
10/04/1994 | US5352954 Plasma generator and associated ionization method |
10/04/1994 | US5352861 Resonant high-voltage pulser for arcjet thruster ignition |
08/24/1994 | EP0611482A1 Ion-optical system for gas discharge ion source. |
08/23/1994 | US5339623 Singly fueled multiple thrusters simultaneously energized by a common power supply |
06/14/1994 | US5319926 Thruster for spacecraft |
05/17/1994 | US5312073 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure and satellite, in particular an electric propulsion satellite, suitable for implementation of the method |
03/16/1994 | EP0587126A1 Long life catalytic gas generator for space propulsion applications |
03/08/1994 | US5291734 Primary force ring for magnetohydrodynamic propulsion system |
03/03/1994 | WO1994005033A1 Ion-optical system for gas discharge ion source |
03/03/1994 | WO1994005032A1 Ion-optical system for gas-discharge ion source |
02/09/1994 | EP0581765A1 Long life arcjet thruster having diffuse cathode arc attachment |
02/03/1994 | WO1994002739A1 Plasma motor with closed electron drift |
02/03/1994 | WO1994002738A1 Fixed plasma motor |
02/03/1994 | CA2139581A1 Fixed plasma motor |
01/18/1994 | CA1326226C Spacecraft with modulated thrust electrostatic ion thruster and associated method |
12/14/1993 | US5269131 Segmented ion thruster |
09/15/1993 | EP0560742A1 Plasma generator and associated ionization method |
08/31/1993 | US5241244 Engine for propelling a vehicle |
08/31/1993 | US5239820 Electric propulsion using C60 molecules |
08/03/1993 | US5231824 Ion beam and ion jet stream motor |
07/07/1993 | EP0550250A1 Propulsion system for spacecraft |
06/08/1993 | US5218271 Plasma accelerator with closed electron drift |
05/18/1993 | US5211006 Magnetohydrodynamic propulsion system |
05/12/1993 | EP0541309A1 Plasma accelerator with closed electron drift |
04/14/1993 | EP0537123A1 Ion generator with ionization chamber constructed from or coated with material with a high coefficient of secondary emission |
04/14/1993 | EP0536736A1 Power supply and control device particularly for RF ion thrustors |
04/07/1993 | EP0535304A1 Arcjet propulsion unit for a space vehicle |
01/13/1993 | EP0522270A1 Arc jet propulsion unit for a space vehicle |
12/23/1992 | EP0519038A1 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure, and a satellite, for implementing same. |
12/15/1992 | US5170623 Hybrid chemical/electromagnetic propulsion system |
11/26/1992 | WO1992009479A3 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure, and a satellite, for implementing same |
11/10/1992 | US5162094 Fusion power generating system |
10/29/1992 | WO1992018983A1 Long life arcjet thruster having diffuse cathode arc attachment |
10/06/1992 | US5152135 Reflector for efficient coupling of a laser beam to air or other fluids |
09/23/1992 | EP0505327A1 Electron cyclotron resonance ion thruster |
09/15/1992 | US5146742 Ion thruster for interplanetary space mission |
09/02/1992 | EP0310664B1 Spacecraft with modulated thrust electrostatic ion thruster and associated method |
05/31/1992 | WO1992009479A2 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure, and a satellite, for implementing same |
05/31/1992 | CA2074959A1 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure and satellite, in particular an electric propulsion satellite, suitable for implementation of the method |
05/19/1992 | CA1301374C Electrostatic ion thruster with improved thrust modulation |
05/12/1992 | US5111656 Arcjet nozzle having improved electrical-to-thrust conversion efficiency and high voltage operation |
01/29/1992 | EP0468706A2 Thrust vector control unit for an ion thruster |
01/08/1992 | EP0464383A2 Plasma neutralisation cathode |
01/02/1992 | EP0463408A2 Plasma accelerator with closed electron drift |
12/31/1991 | US5076051 Long life arcjet thruster having diffuse cathode arc attachment |
10/24/1991 | DE4012742A1 Nuclear rocket drive for high propulsion - with stacked rings of nuclear fuel and moderator material |
07/31/1991 | EP0346458B1 Electrostatic ion thruster with improved thrust modulation |
05/08/1991 | EP0426110A2 Ion thruster for interplanetary space mission |
02/26/1991 | US4995231 Performance arcjet thruster |
02/07/1991 | WO1990014668A3 Cold fusion propulsion apparatus and energy generating apparatus |
01/16/1991 | EP0277203B1 System for controlling the respective emission currents from a plurality of cathodes of an ion source device and ion propulsion motor |
01/16/1991 | CN2069490U High energy-saving ionic engine |
01/10/1991 | DE4013841A1 Drive using repelling power of short circuit - has open current line arranged behind short circuits |
11/29/1990 | WO1990014668A2 Cold fusion propulsion apparatus and energy generating apparatus |
11/07/1990 | EP0148857B1 Ion thruster power-processing unit |
09/04/1990 | CA1273497A1 Emission current control system for multiple hollow cathode devices |
08/16/1990 | DE3900427A1 Arrangement and method for operating rocket motors at increased temperatures |
06/26/1990 | US4937456 Dielectric coated ion thruster |
05/22/1990 | US4926632 Performance arcjet thruster |
04/11/1990 | CN1007539B Emitting current control system of multi-hollow cathodes |