| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 03/18/1993 | WO1993004923A1 Measurement arrangement useful for controlling the attitude of a three-axis stabilized satellite, corresponding evaluation process, regulating system and process |
| 03/18/1993 | WO1993004922A1 Three-axis stabilized, earth oriented satellite and corresponding sun and earth acquisition device_______________________________ |
| 03/18/1993 | WO1993004921A1 Attitude control process and device for a spacecraft to be rotated around a body axis |
| 03/18/1993 | DE4129628A1 Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges Method and apparatus for positioning control of a three-axis stabilized, swirling spacecraft |
| 03/18/1993 | DE4129627A1 Verfahren und vorrichtung zur lageregelung eines um eine koerperfeste achse in rotation zu versetzenden raumfahrzeuges Method and apparatus for positioning control of a koerperfeste axis to-offsetting in rotation spacecraft |
| 03/18/1993 | CA2117094A1 Process and device for controlling the attitude of a three-axis stabilized, spinning spacecraft |
| 03/17/1993 | EP0246226B1 Pointing compensation system for spacecraft instruments |
| 03/16/1993 | US5194872 Inertial navigation system with automatic redundancy and dynamic compensation of gyroscope drift error |
| 03/16/1993 | US5193766 Retry/recovery method in rendezvous maneuver |
| 03/16/1993 | CA1314609C Distributed-array radar system comprising an array of interconnected elementary satellites |
| 03/11/1993 | DE4227070A1 Thermal controller for geosynchronous orbiting spacecraft - has combination of conductive panels and optically reflecting panels on spacecraft surface for thermal balance |
| 03/10/1993 | EP0531055A2 Thrust tube capable of sufficiently damping a vibration |
| 03/09/1993 | US5191761 Aerospace plane and engine |
| 03/04/1993 | WO1993003962A2 Satellite propulsion and power system |
| 03/04/1993 | DE4129096A1 Appts. for radar observation of earth surface - involves flying body in circulating path carrying at least one radio installation, body being unmanned |
| 03/03/1993 | EP0529776A1 Thermal control and electrostatic discharge laminate |
| 03/02/1993 | US5190392 Robot-friendly connector |
| 03/02/1993 | US5190246 Shuttle orbiter with telescoping main propulsion unit and payload |
| 03/02/1993 | US5189773 Mast forming and deployment system |
| 02/16/1993 | US5187805 Telemetry, tracking and control for satellite cellular communication systems |
| 02/16/1993 | US5186567 Quick-connect fasteners for assembling devices in space |
| 02/16/1993 | US5186419 Space transfer vehicle and integrated guidance launch system |
| 02/16/1993 | CA1313698C Spacecraft accelerometer auto-alignment |
| 02/11/1993 | DE4226225A1 Heat transfer pipe with evaporating and condensing sections - has circumferential and longitudinal capillary grooves in wall |
| 02/09/1993 | US5184790 Two-axis attitude correction for orbit inclination |
| 02/09/1993 | US5184789 Space station facility |
| 02/04/1993 | DE4125704A1 Component stack unfolding mechanism |
| 02/03/1993 | EP0526363A2 Composite flexible blanket insulation |
| 02/02/1993 | US5183225 Statite: spacecraft that utilizes sight pressure and method of use |
| 02/02/1993 | CA2075116A1 Composite flexible blanket insulation |
| 01/28/1993 | DE4122687A1 Threaded connector e.g. bolt with overload indication - has easily-deformed plastics indicator medium in gap between nut and washer, with conical contact surface |
| 01/27/1993 | EP0524888A1 Solar sail |
| 01/26/1993 | US5181430 Fine adjustment control mechanism for orientation and/or positioning of a pay load |
| 01/21/1993 | WO1993001090A1 Vehicle propulsion system with external propellant supply |
| 01/20/1993 | EP0524046A1 Device for flexible temporary mechanical attachment with calibrated rupture in tension and method for its manufacture |
| 01/14/1993 | DE4122662A1 High temp. resistant reflecting body for use in space travel - comprising precious metal coating e.g. gold@, platinum@, etc., on ceramic support |
| 01/13/1993 | EP0522954A1 Surface tension vessel with multiple output flow |
| 01/13/1993 | EP0522930A1 Method and device for continuously and unidirectionally controlling the roll-yaw attitude of a satellite |
| 01/13/1993 | EP0522270A1 Arc jet propulsion unit for a space vehicle |
| 01/13/1993 | EP0522241A1 Cooling arrangement for spacecraft |
| 01/12/1993 | US5178347 Process of launching a capsule into space and corresponding launching means |
| 01/10/1993 | CA2072545A1 Continuously acting one-way satellite roll-yaw attitude control method and device |
| 01/10/1993 | CA2072448A1 Temporary mechanical attachment device flexible in bending and designed to fracture at a predetermined tensile load, and method of manufacturing it |
| 01/09/1993 | CA2073262A1 Surface tension tank with multiple delivery rates |
| 01/07/1993 | WO1992021562A3 Solar power system for a space vehicle |
| 01/07/1993 | EP0521364A2 Triaxial laser gyroscope |
| 01/07/1993 | EP0521124A1 Device for unfolding a stack of elements. |
| 01/07/1993 | DE4122185A1 Translatory motion device for space craft - has rotated disc with spiral structures in both surface and spiral arms rotated by translation medium |
| 01/05/1993 | US5177686 Method for determining the position of a space vehicle by means of star acquisition and star identification |
| 01/05/1993 | US5176326 Turbulent droplet generator with boom mounted pitot pump collector |
| 01/05/1993 | US5175975 Compact vacuum insulation |
| 12/30/1992 | EP0520165A1 Momentum wheel platform steering system and method |
| 12/29/1992 | US5174772 Work attachment mechanism/work attachment fixture |
| 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. |
| 12/22/1992 | US5173350 Thermal protection coating comprising a fiber reinforced main layer and an insulative sublayer |
| 12/22/1992 | US5172876 Spin reorientation maneuver for spinning spacecraft |
| 12/22/1992 | US5172875 Space launcher and method for launching objects into space |
| 12/10/1992 | WO1992021562A2 Solar power system for a space vehicle |
| 12/10/1992 | WO1992021561A1 Space transport architecture and method for robotic planetary operations |
| 12/09/1992 | EP0516996A1 Apparatus for controlling fluid flow |
| 12/08/1992 | US5169260 Device for linking two objects by several fixing points |
| 12/08/1992 | US5169094 Geostationary earth observation satellite incorporating liquid propellant apogee maneuver system and hollow antennas |
| 12/08/1992 | US5168673 Method and apparatus for damping vibrations |
| 12/03/1992 | DE4217527A1 Fluid flow regulator suitable for deriving vaporised medium for waste heat in spacecraft - has valve gate connected to end of Bourdon type tube responding to pressure to open and close nozzle |
| 12/02/1992 | EP0516519A1 Selflocking, reversible mechanism for the deployment of a rocket nozzle cone |
| 12/02/1992 | EP0515891A1 Process for producing mouldings from expanded graphite |
| 12/01/1992 | US5167464 Coupling device for joining two items |
| 12/01/1992 | US5167386 Pyrotechnic removal of a radome cover |
| 12/01/1992 | CA2069204A1 Self-locking and reversible mechanism for deploying the diverging portion of a rocket engine nozzle |
| 11/26/1992 | WO1992020576A1 Formationkeeping in a constellation of satellites |
| 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 |
| 11/26/1992 | CA2069219A1 Process for the production of mouldings |
| 11/25/1992 | EP0515072A1 Umbilical release mechanism |
| 11/17/1992 | US5164129 Rolled and flattened compact tube which can be heat activated, foamed and cured to form a rigid construction material, to be transported by the space shuttle for use in assembling orbital structures |
| 11/17/1992 | US5163641 Method and apparatus for changing orbit of artificial satellite |
| 11/17/1992 | US5163640 Active spin axis control for spinning space vehicles |
| 11/17/1992 | US5163262 Collapsible structure |
| 11/17/1992 | CA1310165C Collapsible truss structure |
| 11/12/1992 | WO1992020113A1 Nickel-hydrogen accumulator battery |
| 11/12/1992 | WO1992019498A1 Device for adjusting the position of satellites by means of solar pressure torques |
| 11/12/1992 | DE4114910A1 Drive unit for space vehicle - has double catapult for discharging equal masses in direction of opposing bases of drive housing |
| 11/12/1992 | DE4114804A1 Vorrichtung zur lageregelung von satelliten mit solardruckmomenten Device for positioning control of satellite with solar pressure torques |
| 11/11/1992 | EP0512906A1 Battery of nickel-hydrogen accumulators |
| 11/10/1992 | US5161756 Thermally isolated variable diameter deployable shield for spacecraft |
| 11/10/1992 | US5161610 Evaporation heat exchanger, especially for a spacecraft |
| 11/05/1992 | DE4119588C1 Insert fastener on support in three=dimensionally adjustable position - has fastening units, whose couplers are each positioned independently of insert adjusting position |
| 11/03/1992 | US5159839 Apparatus for gauging high pressure gas, in particular the supply of oxygen gas on board an aircraft |
| 10/29/1992 | WO1992018384A1 Structural latch for vehicle coupling mechanisms |
| 10/28/1992 | EP0510789A1 Cellular telephone satellite system |
| 10/27/1992 | US5158362 Method for measuring the mass of liquid in a storage tank |
| 10/27/1992 | US5158250 Spin-stabilized artificial satellite with passive compensation of solar radiation pressure |
| 10/27/1992 | US5158249 Orbital systems for cislunar travel |
| 10/27/1992 | US5158248 Modular earth-return space vehicle |
| 10/27/1992 | US5158133 Evaporation heat exchanger, especially for a spacecraft |
| 10/27/1992 | US5157893 Compact vacuum insulation |
| 10/27/1992 | US5157816 Interconnection of cylindrical parts |
| 10/23/1992 | CA2040897A1 Mass-energy equivalence space propulsion system |
| 10/22/1992 | DE4112623A1 Fuel tank for rocket motor - is connected to smaller tank which collects residual fuel for further use |
| 10/21/1992 | EP0509640A2 Solid-state imaging device sensitive on two sides |
| 10/21/1992 | EP0509394A1 Seeker head cover for guided missile |