Patents for B64G 1 - Cosmonautic vehicles (11,089)
06/2006
06/28/2006EP1675187A1 Coating for prevention of electrostatic discharge within an equipment in a spatial environment
06/28/2006EP1674392A1 Ejector for spin-stabilised container
06/28/2006EP1674391A1 Ejector for spin-stabilised containers
06/28/2006EP1674390A1 Ejector for spin-stabilised container
06/22/2006WO2006020314A8 Method and system for optimizing torque in a cmg array
06/22/2006US20060136103 Low earth orbit satellite command planning device and method, and low earth orbit satellite control system including the same
06/21/2006EP1461248B1 Space craft with extensible radiators
06/21/2006EP1373071B1 Solar panel with electrical terminals distributed across the surface thereof
06/21/2006CN1789082A Infra-red width difference method for determining posture of on-track geosynchronous spinning satellite
06/21/2006CN1789081A Flying peg-top
06/21/2006CN1260480C Released control release mechanism in space industry
06/20/2006US7063288 Shock wave modification method and system
06/14/2006EP1670301A1 Connection assembly comprising a holder with an aperture and a connector housing mounted on said holder
06/14/2006EP1669587A1 Propulsion system
06/14/2006EP1669292A1 Optimized land mobile satellite configuration and steering method
06/14/2006EP1669291A1 Optimized land mobile satellite system for north american coverage
06/14/2006EP1669155A1 Welding gun
06/14/2006EP1668966A2 Pulsed plasma accelerator and method
06/14/2006EP1436197B1 Surface optical reflector, for space craft such as a geostationary satellite
06/13/2006US7062363 Refinement of spacecraft angular velocity and attitude estimates using star data
06/13/2006US7059571 Deployable spacecraft mount for electric propulsion
06/13/2006US7059094 Frame structure
06/13/2006US7059090 Fairing access door with reinforcement and method of manufacture
06/08/2006WO2006031667A3 Generalized inertial measurement error reduction through multiple axis rotation during flight
06/06/2006US7057734 Integrated reaction wheel assembly and fiber optic gyro
06/06/2006US7055781 Cooled insulation surface temperature control system
06/01/2006WO2006056742A1 Satellite launch system
06/01/2006WO2006056716A1 Assembly for a spacecraft propulsion system and propulsion system comprising at least one such assembly
06/01/2006WO2006056710A1 Resistojet
05/2006
05/31/2006CN1258038C Pressure actuating joint system
05/30/2006US7051981 Method for aligning a spacecraft
05/30/2006US7051980 Efficient orbit sparing system for space vehicle constellations
05/30/2006US7051608 Gyroscopic actuator
05/25/2006US20060110007 Method for detecting linear image in planar picture
05/25/2006US20060108479 Winged spacecraft
05/25/2006US20060107611 Deployable rectangular truss beam with orthogonally-hinged folding diagonals
05/24/2006EP1659063A1 Mixed germanium-silicon thermal control blanket
05/24/2006EP1569847B1 Solar control method for spacecraft
05/24/2006CN2783289Y Multi-channel temperature sampling system for aeronatutics and astronautics system
05/24/2006CN1775629A Flat-clock type spaceship orbital cabin
05/23/2006US7048233 Dual conduction heat dissipating system for a spacecraft
05/18/2006US20060105708 Communication system, communication receiving device and communication terminal in the system
05/18/2006US20060102796 Folding retractable protective dome for space vehicle equipment
05/18/2006US20060102795 Fusion energy system and plasma propulsion aircraft to produce electricity from a controlled nuclear fusion reaction
05/17/2006EP1480878B1 Launch lock for spacecraft payloads
05/17/2006EP1463895B1 Spacecraft isolator launch restraint
05/17/2006CN1772562A Inflating expanded truss for outer space use
05/16/2006US7046934 Optical communication system using a high altitude tethered balloon
05/16/2006US7043925 Densifier for simultaneous conditioning of two cryogenic liquids
05/11/2006WO2006048565A1 Device for controlling the deployment of inflatable structures
05/11/2006US20060100752 Automatic operation system and method for automating satellite control operation and satellite ground control system using the same
05/10/2006EP1655223A2 Satellite dispenser
05/10/2006EP1654159A1 Apparatus for a geosynchronous life extension spacecraft
05/10/2006CN1771421A Heat transfer system
05/10/2006CN1769137A Truss type rigidifying solar energy cell array of inflatable expansion
05/04/2006US20060091491 Optical detector and method of producing an arrangement of multiple semiconductor layers
05/04/2006US20060091262 Method and apparatus for elevating and manipulating objects using electromagnetic fields only
05/04/2006US20060091261 Integrated momentum wall
05/04/2006DE102004063115B3 Spin-stabilized vessel dropping device for spacecraft, has central rope roll placed on ring which serves as holding ring, in which vessel is set in translatory motion when vessel, placed on holding ring, rotates along with holding ring
05/03/2006EP1651853A2 Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits
05/03/2006EP1651518A1 Surface temperature control system
05/03/2006CN2776847Y Non light sensitive region protection structure of anti radiation reinforced charge coupled device
05/03/2006CN1768200A Unitized hybrid rocket system
05/03/2006CN1767977A Winged spacecraft
05/03/2006CN1254408C Non-geostationary satellites constellation, communication system and communication method
05/02/2006US7038203 Method for observing high-altitude neutral air and device for observing high-altitude neutral air
05/02/2006US7036773 Compact external launcher for small space payloads
05/02/2006US7036772 Spacecraft with extensible radiators
05/02/2006US7036423 Released control release mechanism in particular for use in the space industry
05/02/2006CA2183889C Data processor for selecting data elements having the highest magnitude values and storing them in ascending order
04/2006
04/27/2006WO2005103510A3 Non-pyrolytically actuated reduced-shock separation fastener
04/27/2006US20060086865 Momentum tube for distributed actuation
04/27/2006DE102004063116B3 Missile ejection device for space craft, has ring units and twisted towing ropes arranged between ring units, and missile holding and guiding units arranged at ring unit connected with structure of space craft
04/26/2006EP1551710B1 Multi-function reaction wheel assemblies for controlling spacecraft attitude
04/20/2006US20060084334 Method for producing a nonwoven material by hydrodynamic needling
04/20/2006DE102004049826A1 Solar powered drive system for space vehicle operating under weightless conditions employ reaction from contra-rotating rotors
04/19/2006EP1647482A1 Payload ejection system
04/19/2006EP1646843A1 Reaction wheel assembly and fiber optic gyro
04/19/2006CN2773403Y Pneumatic power-back device
04/18/2006US7031653 Switch matrix for satellite payloads with multiple uplink beams and on-board signal processing
04/18/2006US7028953 Two-sided deployable thermal radiator system and method
04/18/2006US7028952 Rotation stabilizing device in a microgravitational rotating apparatus
04/18/2006US7028442 Deployable truss beam with orthogonally-hinged folding diagonals
04/13/2006US20060076459 Isolating positioning boom for instrument platform
04/13/2006US20060076458 Payload module
04/12/2006CN1757565A Mechanism for controlling developing space inflation development structure
04/12/2006CA2481773A1 Electric motor propulsion system
04/11/2006US7025307 Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector
04/11/2006CA2298124C Satellite system and method for setting orbital elements
04/06/2006DE4141166B3 Mechanische Verbindungsvorrichtung zwischen einem keramischen Material und einem Metall, insbesondere zur Verwirklichung einer Steuerflächen-Angriffskante Mechanical connection means between a ceramic material and a metal, in particular for realizing a control surface leading edge
04/04/2006US7021776 Space navigation optical instrument and contaminant removing method thereof
04/04/2006US7021217 Versatile cavity actuator and systems incorporating same
04/04/2006CA2254026C Hybrid electric vehicle with reduced auxiliary power to batteries during regenerative braking
03/2006
03/30/2006US20060065789 Method for producing thrusts with "Mach" effects manipulated by alternating electromagnetic fields
03/30/2006US20060065788 Target acquisition control for spacecraft gimballed payload
03/30/2006US20060065663 High pressure vessel
03/30/2006DE10132723B4 Satellitenkonfiguration zur interferometrischen und/oder tomografischen Abbildung der Erdoberfläche mittels Radar mit synthetischer Apertur (SAR) Satellite configuration for interferometric and / or tomographic imaging of the Earth's surface by means of synthetic aperture radar (SAR)
03/29/2006EP1638766A2 Positive pressure hot bonder
03/29/2006CN1751965A Ultraviolet light rigidization composite film capable of aeration expanding outer space structure
03/28/2006CA2254028C Hybrid electric vehicle with traction motor drive allocated between battery and auxiliary source depending upon battery charge state
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