| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 01/16/2001 | US6174565 By infiltrating only surface portions of a porous ceramic material with a pre-ceramic polymer, curing the infiltrated pre-ceramic polymer and pyrolyzing the polymer; use to protect metallic structure of aircraft from hot exhaust gases |
| 01/16/2001 | US6173923 Power wing |
| 01/16/2001 | US6173922 Failure resistant multiline tether |
| 01/16/2001 | US6173565 Three axis pulsed plasma thruster with angled cathode and anode strip lines |
| 01/11/2001 | WO2001003310A1 Universal replacement communications satellite |
| 01/11/2001 | WO2001002921A2 Momentum position control |
| 01/11/2001 | WO2001002248A1 Method and device for the separation of a satellite from a carrier rocket |
| 01/11/2001 | CA2378157A1 Momentum position control |
| 01/11/2001 | CA2350323A1 Universal replacement communications satellite |
| 01/10/2001 | EP1067630A2 Reflector with resistive taper in connection with dense packed feeds for cellular spot beam satellite coverage |
| 01/10/2001 | EP1067623A2 Deployment of dual reflector systems |
| 01/10/2001 | EP1067446A1 Sytem for satellite attitude control and corresponding method |
| 01/09/2001 | US6170605 Panel for absorbing acoustic energy |
| 01/09/2001 | US6170404 Pressure-driven magnetically-coupled conveyance |
| 01/09/2001 | US6170256 Anchor device for a member for actuating a steerable nozzle |
| 01/09/2001 | CA2034084C Method for controlling east/west motion of a geostationary satellite |
| 01/04/2001 | WO2001001515A1 System comprising a satellite with radiofrequency antenna |
| 01/04/2001 | DE19929746A1 Body cleaner has inflow and outflow pipes, housing-hood, elastic seal, collector and hand-holder |
| 01/03/2001 | EP1065806A2 Universal replacement communications satellite |
| 01/03/2001 | EP1065516A2 Ephemeris/attitude reference determination using on-board optics and other satellite ephemeris |
| 01/03/2001 | EP1065515A2 Ephemeris/attitude reference determination using communications links |
| 01/03/2001 | EP1065450A2 Absorber-reflector for solar heating |
| 01/03/2001 | EP1065389A2 Screw connection for a fibre reinforced ceramic material |
| 01/03/2001 | EP1065141A2 A solar cell assembly |
| 01/03/2001 | EP1064591A2 Continuous spacecraft attitude control that avoids cmg array singularities |
| 01/03/2001 | EP1064198A1 Robust singularity avoidance in satellite attitude control |
| 01/03/2001 | EP1064197A1 Cmg control based on angular momentum to control satellite attitude |
| 01/03/2001 | EP1064196A2 Singularity avoidance in a cmg satellite attitude control |
| 01/02/2001 | US6168116 Shear tie device |
| 12/28/2000 | WO2000079116A1 Rocket thrust chamber |
| 12/28/2000 | WO2000079115A1 Thrust chamber assembly |
| 12/28/2000 | WO2000078610A2 Fly back booster |
| 12/28/2000 | DE19929128A1 Pulse drive has highly flexible metal rope set into mechanical corpuscular vibration by piezo crystals to eject corpuscles that are magnetically accelerated and generate thrust |
| 12/28/2000 | DE19927735A1 Thrust chamber for space travel propulsion units has thermally conducting film at least in area on outside of preparation chamber wall on which fuel forms cooling film before combustion |
| 12/28/2000 | DE19927734A1 Thrust chamber housing for satellite/space transporter propulsion system has combustion nozzle part welded to chamber, expansion nozzle housings via platinum-rhodium alloy rings |
| 12/26/2000 | US6167263 Aerial communications network including a plurality of aerial platforms |
| 12/26/2000 | US6166684 Artificial satellite navigation system and method |
| 12/26/2000 | US6164597 Using reflected solar radiation pressure to provide stationkeeping maneuvering of a spacecraft |
| 12/26/2000 | US6164596 Designs of and methodology for inward or outward, and partially inward or outward turning flow hypersonic air-breathing and rocket-based-combined-cycle vehicles |
| 12/26/2000 | US6164078 Cryogenic liquid heat exchanger system with fluid ejector |
| 12/21/2000 | WO2000077862A1 Spacecraft solar array charging control device |
| 12/14/2000 | DE19958016A1 Plasma generator for plasma coating or machining of large surfaces has all cathodes coupled to voltage source via central current feed line |
| 12/13/2000 | EP1059577A1 Time delay compensation for spacecraft motion compensation |
| 12/13/2000 | EP1059232A2 An orbit raising system and method for geosynchronous satellites |
| 12/13/2000 | EP1059231A2 Solar array control for a satellite with an electric propulsion system |
| 12/13/2000 | EP1059146A2 Modular robot system |
| 12/12/2000 | US6160519 Two-dimensionally steered antenna system |
| 12/12/2000 | US6159271 Separation of gas and liquid, e.g. hydrazine, water, in an orbiting spacecraft by placing magnet(s) in a container opposite a desired location for the diamagnetic liquid; the diamagnetic force repels the liquid to where desired |
| 12/12/2000 | US6158694 Spacecraft inertial attitude and rate sensor control system |
| 12/12/2000 | US6158693 Recoverable booster stage and recovery method |
| 12/12/2000 | US6158187 Collapsible structure |
| 12/12/2000 | US6158088 Deployable hinge assembly providing end of travel damping |
| 12/07/2000 | WO2000047472A3 Air and space vehicle propulsion system |
| 12/07/2000 | DE19924908A1 Dreiachsige Lageregelung für niedrig-fliegende Satelliten Three-axis attitude control for low-flying satellites |
| 12/07/2000 | DE19924851A1 Multiblock-Robot System Multiblock robot system |
| 12/07/2000 | DE19922849A1 Unfolding space travel structure has damping element(s) opposing axle rotation during unfolding until defined rotation angle reached, then unhindered unfolding takes place to final state |
| 12/06/2000 | EP1057503A1 Method for playing a space game and devices for realising this method |
| 12/06/2000 | EP0958170A4 Spacecraft attitude control system using low thrust thrusters |
| 12/05/2000 | US6157161 Low cost battery charging systems |
| 11/30/2000 | DE19921390A1 High precision positioning system for orbiting satellite controls measuring apparatus able to generate by itself signals needed for inertial orientation |
| 11/29/2000 | EP1055600A2 Composite structure element with built-in damping |
| 11/28/2000 | US6154692 Spacecraft yaw pointing for inclined orbits |
| 11/28/2000 | US6154691 Orienting a satellite with controlled momentum gyros |
| 11/28/2000 | US6152403 Gyroscopic calibration methods for spacecraft |
| 11/28/2000 | US6152402 Dual spin zero momentum satellite system |
| 11/28/2000 | US6151900 Cryogenic densification through introduction of a second cryogenic fluid |
| 11/23/2000 | WO2000070252A1 Service valve and use of same in reaction control system |
| 11/23/2000 | WO2000014811A3 Element with electrically controllable surface emissivity for infrared radiation |
| 11/22/2000 | EP1054235A1 Method for determining the co-ordinates of a satellite |
| 11/22/2000 | EP1053604A1 Satellite system |
| 11/21/2000 | US6150995 Combined photovoltaic array and RF reflector |
| 11/21/2000 | US6150660 Staring horizon sensor |
| 11/21/2000 | US6149104 Structural layout for spacecraft including specialized compartment configuration |
| 11/21/2000 | US6149103 Free return lunar flyby transfer method for geosynchronous satellites havint multiple perilune stages |
| 11/21/2000 | US6148740 Load carrying lightweight pallet for spacecraft |
| 11/21/2000 | US6148610 Solid propellant charge for a propulsion unit and propulsion unit equipped with such a charge |
| 11/21/2000 | US6148609 Turbo-rocket thruster |
| 11/21/2000 | CA2117093C Attitude control process and device for a spacecraft to be rotated around a body axis |
| 11/16/2000 | WO2000068630A1 Thermal control system for spacecraft |
| 11/16/2000 | WO2000022291A9 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 11/16/2000 | WO2000013971B1 Fast resonance shifting as a way to reduce propellant for space mission applications |
| 11/15/2000 | EP1051309A2 Method for high-temperature accumulators for stationary energy storage and for actuating nonsystem-connected land, water and air vehicles |
| 11/14/2000 | US6147294 D-wing deployable solar array |
| 11/14/2000 | US6145790 Attitude determination system and method |
| 11/09/2000 | WO2000066425A2 Airship/spacecraft |
| 11/09/2000 | CA2370423A1 Airship/spacecraft |
| 11/08/2000 | EP1050119A1 Dual ring array of satellites |
| 11/07/2000 | US6144334 Method and apparatus for calculating access between satellite constellations and ground targets |
| 11/07/2000 | US6142424 Method of steering a vehicle and vehicle allowing implementation of the method |
| 11/07/2000 | US6142423 Ephemeris/attitude reference determination using on-board optics and other satellite ephemeris |
| 11/07/2000 | US6142422 Method to reorient a spacecraft using only initial single axis attitude knowledge |
| 11/07/2000 | US6142151 Spool valve for switching air flows between two beds |
| 11/02/2000 | WO2000065377A2 Panel for absorbing acoustic energy |
| 11/02/2000 | WO2000064565A2 Spool valve for switching air flows between two adsorption beds |
| 11/02/2000 | EP1048562A2 Emergency exit system |
| 10/31/2000 | US6141606 Wheel speed control system for spacecraft with rejection of null space wheel momentum |
| 10/31/2000 | US6141497 Multilayer micro-gas rheostat with electrical-heater control of gas flow |
| 10/31/2000 | US6138998 Spacecraft antenna slew control systems |
| 10/31/2000 | US6138953 Slew rate direction determination for acquisition maneuvers using reaction wheels |
| 10/31/2000 | US6138952 Transient free actuator switching |