| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 09/27/2005 | CA2367979C Large membrane space structure and method for its deployment and expansion |
| 09/27/2005 | CA2221891C Improvements to observation or telecommunication satellites |
| 09/24/2005 | WO2005090162A1 Passive deployment mechanism for space tethers |
| 09/24/2005 | CA2492887A1 Passive deployment mechanism for space tethers |
| 09/22/2005 | US20050205717 Method of operating a satellite for end-of-life maneuvers |
| 09/21/2005 | CN1219972C Plasma accelerator arrangement |
| 09/20/2005 | US6945500 Apparatus for a geosynchronous life extension spacecraft |
| 09/20/2005 | US6945499 Satellite stand-off tether system |
| 09/20/2005 | US6945498 Commercial experiment system in orbit |
| 09/13/2005 | US6942186 Method and apparatus for propulsion and power generation using spinning electrodynamic tethers |
| 09/13/2005 | US6942016 Heat pipe |
| 09/09/2005 | WO2005083903A1 Method for configuring manhattan street network by low orbit satellites |
| 09/09/2005 | WO2005082714A1 Method for modifying the orientation and local displacement of a space vehicle object and device for carrying out said method |
| 09/09/2005 | WO2005062786A3 Integrated glass ceramic systems |
| 09/08/2005 | US20050193916 Low shock separation joint and method therefore |
| 09/08/2005 | DE102004008681A1 Verfahren zur Energieübertragung mittels kohärenter elektromagnetischer Strahlung A method for power transmission by means of coherent electromagnetic radiation |
| 09/08/2005 | DE102004007024A1 Brake with an arched configuration for a spacecraft comprises an inflatable double-walled structure with at least one airtight chamber formed a tear resistant material |
| 09/08/2005 | DE102004007023A1 Space rope for transporting objects from Earth's surface into the space and vice versa is provided with gas balloons fixed along its length to provide a lift |
| 09/08/2005 | DE102004007019A1 Parachute or an air brake for a spacecraft or a space probe comprises at least one inflatable airtight chamber with a double-walled structure consisting of a tear resistant material |
| 09/08/2005 | DE102004007018A1 Aircraft comprises a fuselage and/or inner elements consisting of a tear resistant material in the form of double-walled structures incorporating airtight inflatable chambers |
| 09/08/2005 | DE102004004543A1 Loading and docking station for spaceships with solar sails has inner ring with clips on large ship or station engaging outer ring on docking probe of tug assembling space debris |
| 09/07/2005 | EP1570531A2 Space-based power system |
| 09/07/2005 | EP1569847A1 Solar control method for spacecraft |
| 09/07/2005 | CN1663885A Loading method of star landing vehicle and equipment for landing |
| 09/07/2005 | CN1663884A Vibration reduction restriction damping layer of spacecraft |
| 09/06/2005 | US6939610 by using phase change materials (PCM); when they reach the temperature at which they change phase they absorb large amounts of heat without getting hotter |
| 09/06/2005 | US6938858 Spacecraft window assembly |
| 09/06/2005 | US6938679 Heat transport apparatus |
| 09/01/2005 | WO2005080198A1 Payload module |
| 09/01/2005 | US20050192719 Navigational system and method utilizing sources of pulsed celestial radiation |
| 09/01/2005 | US20050190427 Method and apparatus for transmitting energy via a laser beam |
| 09/01/2005 | DE10340092B4 Sandwich Struktur mit kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren Sandwich structure with carbon fiber reinforced layers and integrated metallic Kondensierrohren |
| 08/31/2005 | EP1568608A1 Attenuation device |
| 08/31/2005 | EP1492706B1 Spacecraft, method for building such a spacecraft, and adaptor to be used in such a spacecraft |
| 08/31/2005 | EP1064197B1 Cmg control based on angular momentum to control satellite attitude |
| 08/30/2005 | US6937968 Method and apparatus for sequentially profiling and solving problems in space mission analysis |
| 08/30/2005 | US6936760 Space-based power system |
| 08/30/2005 | US6936339 Carbon composites with silicon based resin to inhibit oxidation |
| 08/25/2005 | WO2005077759A1 Reusable space vehicle |
| 08/25/2005 | US20050183377 Deployable and retractable space frame |
| 08/25/2005 | DE19544641B4 Solarzellen-Verbinder für Raumfahrt-Solargeneratoren Solar connector for Space Solar generators |
| 08/25/2005 | DE10393136T5 Al-Cu-Mg-Si Legierung und Verfahren zur Herstellung derselben Al-Cu-Mg-Si alloy and process for producing same |
| 08/25/2005 | DE102004030303A1 Swivel nozzle assembly for steering boat, aircraft or spaceship has partially overlapping rings of progressively decreasing diameter pivoted so as to bend nozzle into curve |
| 08/25/2005 | CA2765417A1 Radiator apparatus |
| 08/24/2005 | EP1566902A1 Method of energy transmission using coherent electromagnetic radiation |
| 08/24/2005 | EP1566679A1 Hinge for deploying the petals of a sectored mirror of an optical space telescope |
| 08/24/2005 | EP1566678A1 Latch for fixing the petal of a sectored optical space telescope mirror |
| 08/23/2005 | US6933334 Silicone-cork ablative material |
| 08/23/2005 | US6932302 Reusable launch system |
| 08/23/2005 | US6931832 Monopropellant combustion system |
| 08/23/2005 | CA2185862C Multiple altitude satellite relay system and method |
| 08/18/2005 | WO2005075938A1 Bearingless gyroscope |
| 08/18/2005 | WO2005075838A2 Protection of surfaces against cavitation erosion |
| 08/18/2005 | WO2005075700A1 Pulsed protection window for applications in pulsed laser deposition |
| 08/18/2005 | WO2004100171A3 In orbit space transportation & recovery system |
| 08/18/2005 | US20050182529 Phase recovery filtering techniques for scp throughput shortage |
| 08/18/2005 | US20050178921 Deployable solar array assembly |
| 08/18/2005 | US20050178920 Spacecraft propulsion system |
| 08/18/2005 | US20050178919 System and method for an ambient atmosphere ion thruster |
| 08/18/2005 | US20050178918 Communication system, communication receiving device and communication terminal in the system |
| 08/18/2005 | US20050178886 Thrust vector actuation control system and method |
| 08/18/2005 | US20050178874 Reflector deployment error estimation |
| 08/18/2005 | DE10318580B4 Verfahren und Empfänger zur gleichzeitigen Erfassung und Auswertung von mindestens zwei elektromagnetischen Signalen Method and receiver for the simultaneous detection and evaluation of at least two electromagnetic signals |
| 08/18/2005 | DE10061773B4 Separationsrahmen zur Trennung mehrerer axial angeordneter Satelliten Separation frame to separate multiple axially arranged satellite |
| 08/16/2005 | US6930654 Deployable antenna reflector |
| 08/11/2005 | WO2005073085A1 In orbit space transportation & recovery system |
| 08/11/2005 | WO2005072220A2 Reversable space plane |
| 08/11/2005 | WO2005039956A3 Vehicle having an articulated suspension and method of using same |
| 08/10/2005 | EP1347916B1 A system and method for implementing a constellation of non-geostationary satellites that provides simplified satellite tracking |
| 08/10/2005 | EP1078400A4 A retractable thin film solar concentrator for spacecraft |
| 08/09/2005 | US6926226 Composite combination for launching a payload into space |
| 08/09/2005 | US6926036 Fluidic diverter valve with a non-spherical shuttle element |
| 08/09/2005 | US6925939 Low shock separation bolt |
| 08/04/2005 | WO2005071512A1 Arc quenching device for a solar array |
| 08/04/2005 | US20050166691 Gyroscope device for creating a precession torque |
| 08/03/2005 | EP1559649A1 Artificial satellite |
| 08/03/2005 | EP1167188A4 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor |
| 08/03/2005 | EP1119741B1 Combined earth/star sensor system and method for determining the orbit and position of spacecraft |
| 08/03/2005 | CN1648002A Space power system principle without mass loss |
| 08/02/2005 | US6923249 Passive thermal control system |
| 08/02/2005 | US6923090 Device for temporarily locking a rotor, in particular a magnetically suspended rotor of an inertia wheel for space applications |
| 07/28/2005 | WO2005068296A1 System and method for adaptive cancellation of disturbances |
| 07/28/2005 | WO2005068295A2 Acoustically damped composite construction for the forward portion of a rocket or missile |
| 07/28/2005 | WO2004079188A3 Drive device pertaining to a space missile and method for controlling the position of a space missile comprising one such drive device |
| 07/28/2005 | WO2004064459A3 Ion accelerator arrangement |
| 07/28/2005 | DE10359208A1 Electro thermal impulse tubing system for spacecraft, has conveyor equipment placed in mirror-image configuration, where changes in state of gas flow are achieved when there is current flow in equipment due to feeding or dissipating heat |
| 07/28/2005 | DE10359184A1 Sensor zur Erfassung der Position der Sonne Sensor for detecting the position of the sun |
| 07/28/2005 | DE10342954B4 Bergungsvorrichtung Saving device |
| 07/27/2005 | EP1557358A1 Thermally activated actuator |
| 07/27/2005 | CN1644456A Miniature assembled gesture measuring system for mini-satellite |
| 07/26/2005 | US6922610 Robot having offset rotary joints |
| 07/26/2005 | US6921051 System for the delivery and orbital maintenance of micro satellites and small space-based instruments |
| 07/26/2005 | US6921050 Solar torque control using thin film directionally reflective, emissive, absorptive and transmissive surfaces |
| 07/26/2005 | US6921049 System for counteracting a disturbance in a spacecraft |
| 07/26/2005 | US6921048 Method and apparatus for minimizing solar array sun tracking disturbance by north and south solar array wing cancellation |
| 07/26/2005 | US6920966 Remotely releasable support strut |
| 07/26/2005 | US6920733 Unfoldable connected structure and method for unfolding the same |
| 07/26/2005 | US6920722 Elongated truss boom structures for space applications |
| 07/21/2005 | US20050156083 Sequencing device for deploying a structure as a function of the kinematics of one mobile body thereof |
| 07/20/2005 | CN1641200A Elastomerized phenolic resin ablative insulation for rocket motors |