| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 10/09/2004 | CA2464035A1 Apparatus and method for servicing and inspecting small free-flying platforms in orbit in space |
| 10/07/2004 | WO2004086079A1 Method and device for assigning weighting coefficients for performing attitude calculations with a star sensor |
| 10/07/2004 | WO2004085252A2 Unitized hybrid rocket system |
| 10/07/2004 | US20040195431 Hard shell lighter than air orbiter |
| 10/07/2004 | US20040194397 Elongated truss boom structures for space applications |
| 10/06/2004 | EP1463895A1 Spacecraft isolator launch restraint |
| 10/06/2004 | CN2646053Y Spaceflight flying saucer capable of power-propelled flight in space |
| 10/05/2004 | US6799742 Solar panel for space and method for manufacturing the same |
| 09/30/2004 | US20040188568 Modular architecture for thermal control in a spacecraft |
| 09/30/2004 | US20040188562 Commercial experiment system in orbit |
| 09/30/2004 | US20040187906 Solar generator panel and a spacecraft including it |
| 09/29/2004 | EP1461248A1 Space craft with extensible radiators |
| 09/23/2004 | US20040185776 Digital beacon asymmetry and quantization compensation |
| 09/23/2004 | US20040183452 Plasma-accelerator configuration |
| 09/22/2004 | EP1460048A1 HEAT−RESISTANT MATERIAL AND HOT STRUCTURE MEMBER BOTH FOR SPACE SHUTTLE, SPACE SHUTTLE, AND METHOD FOR PRODUCING HEAT−RESISTANT MATERIAL FOR SPACE SHUTTLE |
| 09/22/2004 | EP1459980A1 Method of computer-assisted determination of a fuel optimum control of nozzles |
| 09/22/2004 | EP1169618B1 An angular rate and reaction torque assembly |
| 09/21/2004 | US6795687 Elliptical satellite system emulating characteristics of geosynchronous satellites during the apogee portion of an elliptical orbit |
| 09/21/2004 | US6793183 Integral node tubular spaceframe |
| 09/21/2004 | CA2210117C One piece spacecraft frame |
| 09/16/2004 | WO2004079188A2 Drive device pertaining to a space missile and method for controlling the position of a space missile comprising one such drive device |
| 09/16/2004 | WO2004049538A3 Space-based power system |
| 09/16/2004 | US20040181319 Method and apparatus for stepping space craft mechanisms at low disturbance rates |
| 09/16/2004 | US20040180242 ceramic material in which silicon carbide is contained in zirconium boride |
| 09/16/2004 | DE10318925A1 Antriebsvorrichtung eines Raumflugkörpers und Verfahren zur Lagesteuerung eines Raumflugkörpers mit einer solchen Antriebsvorrichtung Drive device of a spacecraft attitude control and method for a spacecraft having such a drive device |
| 09/16/2004 | DE10318514B3 Multiple layer ceramic composite material used as a heat-resistant electromagnetic window comprises an oxidic carbon-free fiber-reinforced ceramic layer, and a layer made from a thermal insulating layer consisting of a pure oxidic foam |
| 09/16/2004 | DE10309827A1 Lift drive for helicopter, for example, has at least two masses cardanically mounted on both sides on pivots, whereby pivots for producing of required lifting movement are adjustable from parallel position to relative angled position |
| 09/14/2004 | US6791510 Inflatable structure, array antenna with inflatable structure, and deployment method for inflatable structure |
| 09/14/2004 | US6789767 Active satellite dispenser for reusable launch vehicle |
| 09/09/2004 | US20040176883 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same |
| 09/09/2004 | US20040176881 Apparatus and method for estimating attitude using inertial measurement equipment |
| 09/09/2004 | US20040173257 Space-based power system |
| 09/09/2004 | US20040173037 Gyroscopic actuator |
| 09/08/2004 | EP1334220B1 Material for thermally loaded substrates |
| 09/08/2004 | CN1165993C Retractable thin film solar concentrator for spacecraft |
| 09/07/2004 | US6786669 Positive lock quick release pin |
| 09/07/2004 | US6786456 Deployable inflatable boom and methods for packaging and deploying a deployable inflatable boom |
| 09/02/2004 | WO2004075372A2 An inertia generator or anti-gravitational rotor |
| 09/02/2004 | WO2004074101A1 Satellite electric charge buildup monitor |
| 09/02/2004 | WO2004007287A3 Integrated inertial stellar attitude sensor |
| 09/02/2004 | DE10300728B3 Ionenbeschleuniger-Anordnung Ion accelerator arrangement |
| 09/02/2004 | CA2516110A1 Satellite electric charge buildup monitor |
| 09/01/2004 | EP1452830A1 Gyroscopic actuator |
| 09/01/2004 | EP1156960B1 Autonomous stratospheric airship |
| 08/31/2004 | US6784359 Apparatus and method for the design and manufacture of foldable integrated device array stiffeners |
| 08/26/2004 | WO2004071869A1 Device for controlling the attitude of a satellite by means of gyroscopic actuators |
| 08/26/2004 | US20040167683 Method and device for controlling satellite attitude and steering using a gyrodyne cluster |
| 08/26/2004 | US20040166814 Satellite charge monitor |
| 08/26/2004 | US20040164205 Deployable spacecraft mount for electric propulsion |
| 08/26/2004 | US20040163869 Articulated vehicle suspension system shoulder joint |
| 08/26/2004 | US20040163863 Hub drive and method of using same |
| 08/26/2004 | US20040163699 Solar cell for a solar generator panel, a solar generator panel, and a space vehicle |
| 08/25/2004 | EP1448477A2 Composites based on carbon nanotubes or nanofibers deposited on an activated support for use in catalysis |
| 08/25/2004 | EP1448369A1 Method and system of thermal protection |
| 08/24/2004 | US6779759 Integrated power and attitude control system and method |
| 08/18/2004 | EP1366986A4 Device for jettisoning large heavy freights from an aircraft |
| 08/18/2004 | EP1299673A4 Method and system for densifying cryogenic propellants |
| 08/18/2004 | EP1044352B1 Rotational speed measurement device for rotating missiles |
| 08/17/2004 | US6776375 Payload deployment system with an internal cargo unit |
| 08/17/2004 | US6776372 Method of operating a satellite for end-of-life maneuvers |
| 08/17/2004 | US6776258 Acoustic blanket system |
| 08/17/2004 | US6776220 Spacecraft radiator system using crossing heat pipes |
| 08/13/2004 | CA2418641A1 Prototype starship propulsion system |
| 08/12/2004 | US20040157518 Method of fabricating reusable surface insulation containing polybenzazole |
| 08/12/2004 | US20040156673 Apparatus for releasably interconnecting structural components having a rotational symmetry |
| 08/11/2004 | EP1445440A1 Method and apparatus for thermal management of vehicle exhaust systems |
| 08/10/2004 | US6775600 Systems and methods for determining a spacecraft orientation |
| 08/10/2004 | US6775599 Multi-function reaction wheel assemblies for controlling spacecraft attitude |
| 08/10/2004 | US6772978 Dynamic unbalance compensation system and method |
| 08/10/2004 | US6772517 Heat insulating material |
| 08/05/2004 | WO2004022867A3 Stiffener reinforced foldable member |
| 08/05/2004 | US20040149861 S & H Cycle Engine |
| 08/05/2004 | US20040149860 Laser guidance system |
| 08/05/2004 | US20040149485 Cable for a space elevator |
| 08/05/2004 | US20040149421 Soldering of saddles to low expansion alloy heat pipes |
| 08/05/2004 | DE10302717A1 Optical receiver used in a spacecraft has the incident emission received measured by sensors to provide input to controller input |
| 08/05/2004 | DE10301783A1 Vorrichtung zum lösbaren Verbinden rotationssymmetrischer Bauteile Apparatus for releasably connecting rotationally symmetrical parts |
| 08/04/2004 | EP1442342A1 Autonomous manoeuvring for spinning spacecraft |
| 08/03/2004 | US6769830 Connector assembly |
| 08/03/2004 | US6769690 Mechanism for independently moving segments of a three-dimensional object and applications thereof |
| 08/03/2004 | US6769651 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it |
| 08/03/2004 | US6769242 Rocket engine |
| 08/03/2004 | US6769241 Description of methods to increase propellant throughput in a micro pulsed plasma thruster |
| 07/29/2004 | WO2004064459A2 Ion accelerator arrangement |
| 07/29/2004 | WO2004063009A1 Solar control method for spacecraft |
| 07/29/2004 | US20040148068 Mitigation of angular acceleration effects on optical sensor data |
| 07/29/2004 | US20040144921 Method for observing high-altitude neutral air and device for observing high-altitude neutral air |
| 07/29/2004 | US20040144102 Anti-icing fluid injection nozzle |
| 07/28/2004 | EP1441221A1 Method and device for observing the atmosphere within an altitude range of about 100 km - 1000 km |
| 07/28/2004 | EP1268277A4 Passive, multi-axis, highly damped, shock isolation mounts |
| 07/28/2004 | EP1196326B1 Method and device for integrating satellites on a launcher |
| 07/27/2004 | US6768582 System for deploying the petals of a sectored mirror of an optical space telescope |
| 07/27/2004 | US6766987 Satellite system and method of deploying same |
| 07/22/2004 | US20040140930 Ranging system for determining ranging information of a spacecraft |
| 07/22/2004 | US20040140403 Asymetric gravitational wave propulsion system |
| 07/22/2004 | US20040140402 Solar torque control using thin film directionally reflective, emissive, absorptive and transmissive surfaces |
| 07/22/2004 | US20040140401 System and method for controlling the attitude of a flying object |
| 07/22/2004 | US20040140400 System and method for increasing the roll offset operating range for a spacecraft |
| 07/22/2004 | US20040140399 Method and apparatus for minimizing solar array sun tracking disturbance by north and south solar array wing cancellation |
| 07/21/2004 | EP1439124A2 Device for the releasable connection of rotation-symmetric parts |