| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 03/30/2000 | WO2000017051A1 Holding and releasing mechanism with a shape memory actuator |
| 03/30/2000 | WO2000017050A2 Automated fuel tank assembly system and method |
| 03/30/2000 | DE19840183C1 Element mit elektrisch einstellbarer Oberflächenemissivität für Infrarotstrahlung Element with electrically adjustable surface emissivity for infrared radiation |
| 03/30/2000 | CA2345290A1 Temperature-controlled wire support |
| 03/30/2000 | CA2344684A1 Holding and releasing mechanism with a shape memory actuator |
| 03/29/2000 | EP0988446A1 Device for anchoring a member activating an adjustable nozzle |
| 03/28/2000 | US6042240 Adjustable three dimensional focal length tracking reflector array |
| 03/28/2000 | US6042058 Stationkeeping and momentum-dumping thruster systems and methods |
| 03/28/2000 | US6042057 Aerodynamically actuated magnetic ascent vent cover |
| 03/23/2000 | WO1999065769A3 Electrical drive system for rocket engine propellant pumps |
| 03/22/2000 | EP0987178A2 Element for surface temperature control |
| 03/22/2000 | EP0928269A4 Vehicle rotation and control mechanism |
| 03/21/2000 | US6039290 Robust singularity avoidance in satellite attitude control |
| 03/21/2000 | US6038736 Hinge for deployable truss |
| 03/21/2000 | CA2032808C Attitude control device using solar sails for a satellite stabilized on three axes |
| 03/16/2000 | WO2000014811A2 Element with electrically controllable surface emissivity for infrared radiation |
| 03/16/2000 | WO2000013971A2 Fast resonance shifting as a way to reduce propellant for space mission applications |
| 03/16/2000 | DE19846327C1 Recoverable small aerodynamic vehicle dispatched by parent space vehicles for monitoring, inspecting and repairing tasks has a modular construction under a spherical, flexible external capsule |
| 03/14/2000 | US6038499 Direction detecting device for detecting direction of space vehicle |
| 03/14/2000 | US6037909 Deployed payload for a communications spacecraft |
| 03/14/2000 | US6036144 Mass producible launch system |
| 03/14/2000 | US6036143 Solar array-mounted stationkeeping and maneuvering thrusters |
| 03/09/2000 | WO2000013169A2 Composite fairing with integral damping and internal helmholz resonators |
| 03/09/2000 | WO2000012269A2 Moment control unit for spacecraft attitude control |
| 03/09/2000 | DE19828315C1 Vorrichtung zum Aufbringen oder Absenken einer Vorspannkraft an einem Niederhalterpunkt eines Niederhaltersystems für entfaltbare Bauteile Apparatus for applying or lowering a biasing force on a hold-down device point of a system for deployable components |
| 03/08/2000 | EP0984511A2 Combined photovoltaic array and RF reflector |
| 03/08/2000 | CN1246831A Geostationary satellite stabilised alone three axes with improved temperature control |
| 03/07/2000 | US6034322 Solar cell assembly |
| 03/07/2000 | US6032904 Multiple usage thruster mounting configuration |
| 03/07/2000 | US6032903 Cooperative control structures and methods for satellite spin axis control |
| 03/07/2000 | US6032902 Constellation of non-geostationary satellites providing permanent coverage |
| 03/07/2000 | CA2006463C Device for tightly attaching a fragile object |
| 03/02/2000 | WO2000011754A1 Improved two-dimensionally steered antenna system |
| 03/02/2000 | WO2000011415A2 Adaptively positioned solar array |
| 03/02/2000 | WO2000011338A1 Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the same |
| 03/02/2000 | DE19839164A1 Method of correcting the center of gravity of a spacecraft involves moving isostatically attached masses parallel to all three axes of the spacecraft, gives high accuracy |
| 02/29/2000 | US6031486 Method and apparatus for integration and testing of satellites |
| 02/29/2000 | US6031178 System to link the kinematics of neighboring panels in a panel assembly |
| 02/29/2000 | US6029935 Method for adding a geostationary component to a non-geostationary satellite network |
| 02/29/2000 | US6029932 Detonating valve for releasing openings of air bag landing systems |
| 02/29/2000 | US6029928 Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft |
| 02/29/2000 | US6029438 Drive circuit for electric propulsion thruster |
| 02/24/2000 | WO2000010207A1 Flexible, foldable solar generator for spacecrafts |
| 02/24/2000 | WO2000009396A2 Multiple spacecraft carrier on launcher |
| 02/24/2000 | DE19859212C1 Space flight structure beam has rolled carbon fibre composite layers with defined angles of weave |
| 02/24/2000 | DE19842102C1 Element for controlling the temperature of a surface in satellites and spacecraft has a functional layer consisting of an IR-transparent matrix material with embedded microparticles |
| 02/24/2000 | DE19836602A1 Modularer Satellit Modular Satellite |
| 02/22/2000 | US6028570 Folding perimeter truss reflector |
| 02/22/2000 | US6027077 Spacecraft with all-cryogenic electronics |
| 02/22/2000 | US6027076 Method for powering a spacecraft with extended-life battery operation |
| 02/22/2000 | US6027072 Payload chamber cooling system |
| 02/17/2000 | WO2000008536A1 Automatic tripping cryo-heat flow switch |
| 02/17/2000 | WO1999061773A3 Anti-slosh liquid propellant tank for launch vehicles |
| 02/17/2000 | DE19836272A1 Flexible, foldable solar generator for spacecraft, contg. foldable array(s) with integrated system of current conductor strips and blankets carrying solar cells |
| 02/16/2000 | EP0979776A1 Robotically drivable interface mechanism |
| 02/16/2000 | EP0979775A2 Modular satellites in satellite formation |
| 02/16/2000 | EP0979774A1 Method for simultaneously launching multiple satellites into orbit |
| 02/15/2000 | US6026337 Microbolometer earth sensor assembly |
| 02/15/2000 | US6025815 Drive unit for adjusting satellite components requiring orientation |
| 02/15/2000 | US6024810 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 02/15/2000 | US6024328 Satellite control method using single species of bipropellant |
| 02/15/2000 | US6024327 Method and apparatus for intelligent attitude and orbit control onboard a satellite |
| 02/10/2000 | WO1999060860A3 Shape memory alloy hinge assembly |
| 02/10/2000 | DE19835305A1 Selbstauslösender Kryo-Wärmestromschalter Automatically firing cryogenic heat flow switch |
| 02/09/2000 | EP0977687A1 Method for low-fuel, computer-assisted control of any number of thrusters arranged on a spacecraft |
| 02/09/2000 | EP0977686A1 Satellite inclination changes using weak stability boundaries |
| 02/08/2000 | US6021979 Sun-referenced safe-hold control for momentum biased satellites |
| 02/03/2000 | WO2000005549A1 System and method for spacecraft attitude control |
| 02/03/2000 | WO2000005134A2 Spacecraft shading device |
| 02/03/2000 | CA2338459A1 System and method for spacecraft attitude control |
| 02/02/2000 | EP0977273A1 Solar reflector systems and methods |
| 02/02/2000 | EP0976655A1 Thin-film reflectors for concentration solar array |
| 02/01/2000 | US6020956 Pseudo gyro |
| 02/01/2000 | US6019320 Spacecraft acquisition of sun pointing |
| 02/01/2000 | US6019319 Momentum wheel energy storage system using magnetic bearings |
| 02/01/2000 | US6019318 Coordinatable system of inclined geosynchronous satellite orbits |
| 01/27/2000 | DE19934511A1 Self-latching deployment apparatus for a multi-paneled solar array |
| 01/26/2000 | EP0974516A2 Spacecraft camera image navigation and registration |
| 01/26/2000 | CN1242324A Elastically deformable antenna reflector for spacecraft, and spacecraft including such reflector |
| 01/25/2000 | US6017013 Damped instrument kinematic mounts |
| 01/25/2000 | US6017003 Satellite operating system and method |
| 01/25/2000 | US6017002 Thin-film solar reflectors deployable from an edge-stowed configuration |
| 01/25/2000 | US6017001 Controlling rotation of a spacecraft |
| 01/25/2000 | US6017000 Apparatus and methods for in-space satellite operations |
| 01/25/2000 | US6016999 Spacecraft platforms |
| 01/18/2000 | US6015116 Fuel efficient methods for satellite stationkeeping and momentum dumping |
| 01/18/2000 | US6014987 Anti-vortex baffle assembly with filter for a tank |
| 01/12/2000 | EP0970884A2 Battery management method for spacecraft |
| 01/12/2000 | EP0970528A1 Electrostatic derivation for solar cells |
| 01/11/2000 | US6012680 Passive lateral vibration isolation system for a spacecraft launch vehicle |
| 01/06/2000 | WO2000001206A1 Plasma accelerator arrangement |
| 01/05/2000 | EP0786096B1 Method for evaluating the non-euclidean effects affecting an image produced by a satellite radar and satellite for carrying out said method |
| 01/04/2000 | US6012000 Simplified onboard attitude control based on star sensing |
| 01/04/2000 | US6011913 Method and apparatus for determination of spacecraft drag |
| 01/04/2000 | US6010096 Deployment restraint and sequencing device |
| 12/30/1999 | DE19828704A1 Plasma accelerator for space vehicles, increasing ion thruster motor efficiency |
| 12/29/1999 | WO1999067132A1 Device for applying or reducing a prestressing force on a holding-down point of a holding-down system for deployable parts |
| 12/29/1999 | CN1239841A Elastically deformable antenna reflector for spacecraft |
| 12/28/1999 | US6008448 Solar panel array with stepped taper |
| 12/28/1999 | US6008447 Transmission for moving panels provided with solar cells on a spacecraft |