Patents for B64G 1 - Cosmonautic vehicles (11,089)
03/2002
03/20/2002EP1188668A1 Orientation device and on-board orientation system
03/20/2002EP1188098A2 Momentum position control
03/20/2002EP1187979A1 Rocket thrust chamber
03/20/2002EP1187978A1 Thrust chamber assembly
03/19/2002US6357700 Electrically powered spacecraft/airship
03/19/2002US6357699 Device for controlled release of tension
03/19/2002US6357698 Twin lobe spacecraft dispenser apparatus and method
03/14/2002WO2002021185A1 Spin-stabilized film mirror and its application in space
03/14/2002WO2002020346A2 An asymmetric gravitational wave propulsion system
03/14/2002US20020032525 GPS receiving system
03/14/2002US20020032115 2For use in manufacture of bodies of space craft and next generation supersonic aircraft, engine parts and gas turbines
03/14/2002US20020030624 Method of and system for receiving microwave
03/14/2002US20020029797 Space photovoltaic power generation method and system
03/14/2002US20020029796 Space photovoltaic power generation system, power satellite, and electric power base
03/14/2002DE10102330C1 Mechanical support structure has memory alloy component providing increased mechanical rigidity in one state and reduced thermal conductivity in second state
03/14/2002DE10043268A1 Heat and aerodynamic protection for returning spacecraft involves empty rocket stage fuel tank as divided casing housing return capsule or recovery vehicle or rocket drive for cost reduction.
03/13/2002EP1186981A2 Offline apparatus for detecting attitude of artificial satellite in wide-band and method thereof
03/12/2002US6356815 Stellar attitude-control systems and methods with weighted measurement-noise covariance matrices
03/12/2002US6356814 Spacecraft magnetic torquer feedback system
03/12/2002US6356245 Microwave strip transmission lines, beamforming networks and antennas and methods for preparing the same
03/12/2002US6354540 Androgynous, reconfigurable closed loop feedback controlled low impact docking system with load sensing electromagnetic capture ring
03/12/2002US6354535 Autonomous stratospheric airship
03/12/2002US6354163 Mitigating gimbal induced disturbances in CMG arrays
03/07/2002WO2002018208A2 Spacecraft sunshield for use in performing solar torque balancing
03/07/2002WO2001054981A3 Propulsion module
03/07/2002US20020027131 Thermal control apparatus and method for thermally controlling a plurality of objects within a predetermined temperature range
03/07/2002DE10040755A1 Fuel tank for corrosive space rocket propellants has removal device in form of refillable reservoir at bottom of tank and connected by supply lines to tank interior
03/06/2002EP1184768A2 Thermal control apparatus and method for thermally controlling a plurality of objects within a predetermined temperature range
03/06/2002EP1184280A2 Deployable carrier structure made of deformable tube elements
03/06/2002CN1080229C System for attaching and separating satellites
03/05/2002US6352397 Reduced shock separation fastener
03/05/2002US6352222 Satellite, satellite control method and satellite communication system
03/05/2002US6351939 Swirling, impinging sheet injector
02/2002
02/28/2002WO2002016204A1 Employing booster trajectory in a payload inertial measurement unit
02/28/2002US20020023987 Support structure having alternative states of high strength or low thermal conductivity, and connecting strut
02/28/2002US20020023427 Micro-colloid thruster system
02/28/2002DE10036840A1 Electrostatic gripping device, esp. for space vehicle, includes source for generating electrostatic field
02/27/2002EP1181503A1 Autonomous satellite navigation system
02/27/2002CN1337912A Payload carry and Launch system
02/27/2002CN1079764C Apparatus and method for operating heat pipe panel assembly under gravity condition
02/26/2002US6350944 Solar module array with reconfigurable tile
02/21/2002WO2000065377A9 Panel for absorbing acoustic energy
02/21/2002US20020020785 Spacecraft orbit control using orbit position feedback
02/21/2002DE10109509A1 Verfahren und Vorrichtung zum Positionieren von Satelliten in eine niedrige Erdumlaufbahn Method and device for positioning of satellites in low Earth orbit
02/19/2002US6349195 Supplemental satellite communication enhancement techniques
02/19/2002US6347766 Method and apparatus for generating propulsive forces without the ejection of propellant
02/19/2002CA2188393C A device for controlling a spacecraft by gating gas via a moving nozzle
02/19/2002CA2188341C System for controlling a space vehicle by gating gas
02/19/2002CA2117090C Measurement arrangement useful for controlling the attitude of a three-axis stabilized satellite, corresponding evaluation process, regulating system and process
02/14/2002WO2001038171A3 Methods and systems for a solar cell concentrator
02/14/2002US20020018333 Apparatus and method for generating gravitational force/gravitational field
02/14/2002US20020017593 Virtually geostationary satellite array
02/14/2002DE10038119A1 Heat flow switch for joining and separating thermally conductive elements to comprises a switching cylinder joined to a heat source, and a corresponding base plate joined to a heat sink
02/13/2002EP1179474A1 Satellite comprising an observation instrument and a solar shade decoupled from each other
02/13/2002EP1179132A1 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines
02/13/2002EP1179131A1 An apparatus for controlling the flow separation line of rocket nozzles
02/12/2002US6347262 Minimum fuel attitude and nutation controller for spinning spacecraft
02/12/2002US6345963 Pump with positive displacement
02/12/2002US6345789 Method and apparatus for propulsion
02/12/2002US6345788 Composite structure element with built-in damping
02/12/2002US6345482 Open-lattice, foldable, self-deployable structure
02/07/2002WO2002010535A2 Iso-truss structure
02/07/2002WO2002010015A1 Modular reaction wheel assembly to shield electronics on a satellite
02/07/2002US20020014558 Reusable, separable, structural connector assembly
02/07/2002CA2417410A1 Modular reaction wheel assembly to shield electronics on a satellite
02/06/2002EP1178334A1 Satellite constellation for measuring atmospheric wind using doppler lidar principles
02/05/2002US6343770 Reusable, separable, structural connector assembly
02/05/2002US6343464 Solar thermal rocket
02/05/2002US6343442 Flattenable foldable boom hinge
02/05/2002CA2117114C Method of manufacturing thermal shielding elements, in particular for space planes
01/2002
01/31/2002WO2002008059A1 Spacecraft capture and docking system
01/31/2002WO2002008058A1 Solar concentrator
01/31/2002WO2001056884A3 Frangible actuator with redundant power supply
01/31/2002WO2001049084A3 Method and apparatus for converting electrostatic potential energy
01/31/2002US20020011033 Building for containing human occupants in an adverse arctic or antarctic environment and structures for containing and protecting occupants in an adverse environment
01/30/2002EP1175332A2 Airship/spacecraft
01/30/2002CN2474995Y Photoelectric sensor
01/30/2002CN1078660C Thermal management of vehicle exhaust systems
01/29/2002US6342865 Side-fed offset cassegrain antenna with main reflector gimbal
01/29/2002US6341762 Service valve and use of same in reaction control system
01/29/2002US6341750 Spacecraft motion estimation using a gimballed momentum wheel
01/29/2002US6341749 Method of simultaneously reducing inclination and eccentricity for geostationary orbit transfer
01/29/2002US6341748 Emergency exit system
01/24/2002WO2002006120A1 Apparatus for imparting unidirectional motion
01/24/2002WO2002006119A1 Multistage modularised boost rocket
01/24/2002WO2001098143A8 Linear electromagnetic propelling device with open magnetic cores
01/24/2002WO2001045293A3 Satellite relay method and apparatus
01/24/2002US20020007845 Solar concentrator
01/24/2002DE10033093A1 Vorrichtung zum lösbaren verbinden rotationssystemmetrischer Bauteile Means for releasably connecting rotationssystemmetrischer components
01/23/2002EP1174342A1 Solar concentrator
01/23/2002EP1173874A1 Plasma gun and methods for the use thereof
01/23/2002EP0963259B1 Solar reflectors
01/22/2002US6341250 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
01/22/2002US6341249 Autonomous unified on-board orbit and attitude control system for satellites
01/22/2002US6340138 Stationkeeping method utilizing open-loop thruster pulses and closed-loop authority limited momentum storage devices
01/22/2002US6340137 Moment control unit for spacecraft attitude control
01/17/2002US20020007233 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
01/17/2002US20020005469 Micro sun sensor using a hologram
01/17/2002DE10031542A1 Inertialsensor zur Lagerung und Kontrolle einer Inertialreferenz in einem Satelliten Inertial sensor for storage and control of inertial reference in a satellite
01/16/2002EP1172294A2 Sun-seeking solar array control system and method
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