| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 03/23/2006 | US20060063529 Sub-orbital, high altitude communications system |
| 03/23/2006 | US20060060718 Radiation shield |
| 03/23/2006 | US20060060717 Fixed satellite constellation system employing non-geostationary satellites in sub-geosynchronous elliptical orbits with common ground tracks |
| 03/23/2006 | US20060060716 Passive deployment mechanism for space tethers |
| 03/23/2006 | US20060060715 Protective shield assembly for space optics and associated methods |
| 03/23/2006 | US20060060702 Cooled insulation surface temperature control system |
| 03/22/2006 | EP1159192B1 Fluid transfer system |
| 03/21/2006 | US7016674 Slice based architecture for a multifunction radio |
| 03/21/2006 | US7014915 Controlled binary macrosegregated powder particles, their uses, and preparation methods therefor |
| 03/21/2006 | US7014150 Method and system for optimizing torque in a CMG array |
| 03/21/2006 | CA2254027C Electric vehicle with variable efficiency regenerative braking depending upon battery charge state |
| 03/21/2006 | CA2254025C Electric vehicle with battery regeneration dependent on battery charge state |
| 03/16/2006 | WO2006028980A2 Space manufacturing module system and method |
| 03/16/2006 | WO2006026958A1 Floating start installation for a space projectile |
| 03/16/2006 | US20060054767 Dynamic kinematic mount |
| 03/16/2006 | US20060054745 Thermal deformation determination for payload pointing using space-based beacon |
| 03/16/2006 | DE102005038697A1 Method for launching of manned or unmanned space probes entails creating connection to geostatic space station which hauls payload to defined height, and from there payload is launched under own power tangentially to space station |
| 03/09/2006 | US20060049317 Articulated assembly of solar generator panels and space vehicle |
| 03/09/2006 | US20060049316 Operating method for launch rockets and a set of rocket boosters for carrying out said method |
| 03/09/2006 | US20060049315 Precision attitude control system for gimaled thruster |
| 03/09/2006 | US20060049314 Quantized control- moment gyroscope array |
| 03/09/2006 | DE202006000022U1 Reaction wheels arranging device for use on pico satellites, has gyroscopic wheels mounted on tetrahedron-shaped base body, where three wheels are provided for attitude stabilization in three degrees of freedom of rotation |
| 03/09/2006 | DE202005015431U1 Reaction wheel arrangement for micro satellite, has precision ball bearings mounted into housing, rotation axis that carries oscillating weight, where arrangement of axis, weight and magnet disc is statically and dynamically balanced |
| 03/08/2006 | EP1519833B1 Product and method for producing a non-woven fabric by means of hydrodynamic needling |
| 03/07/2006 | US7007896 Shock and vibration isolation system |
| 03/02/2006 | DE10227968B4 Lagerungssystem in einem Raumfahrzeug Storage system in a spacecraft |
| 03/01/2006 | EP1628936A2 Explosive devices |
| 03/01/2006 | CN1742379A Space-based power system |
| 03/01/2006 | CN1741936A Ion accelerator arrangement |
| 03/01/2006 | CN1243897C Iso-truss structure |
| 02/28/2006 | US7003941 Thruster device responsive to solar radiation and associated methods |
| 02/23/2006 | WO2006020062A2 A flexible, deployment rate damped hinge |
| 02/23/2006 | US20060038085 Catalyzed decomposing structural payload foam |
| 02/23/2006 | US20060038084 Methods and systems for advanced spaceport information management |
| 02/23/2006 | US20060038083 Power generating and distribution system and method |
| 02/23/2006 | US20060038082 Thermal design for spacecraft modules |
| 02/23/2006 | US20060038081 Electric dipole spacecraft |
| 02/23/2006 | US20060038080 Solar control method for spacecraft |
| 02/23/2006 | US20060037998 Thermally-controlled actuator device |
| 02/22/2006 | CN1737367A Novel jet-propeller and application thereof |
| 02/21/2006 | US7001127 Non-pyrolytically actuated reduced-shock separation fastener |
| 02/21/2006 | US7000308 Method of constructing a rotor for a gyroscopic device |
| 02/16/2006 | WO2005029927A3 Pulsed plasma accelerator and method |
| 02/16/2006 | US20060032986 Reusable thrust-powered sled mounted on an inclined track for launching spacecraft and airborne vehicles at supersonic speeds |
| 02/16/2006 | US20060032985 Clutch driven reaction wheel steering unit |
| 02/15/2006 | EP1626319A1 Dynamic system for controlling mobile apparatuses |
| 02/14/2006 | US6999860 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same |
| 02/14/2006 | US6997416 Linear actuation device for spacecraft and solar generator unfolding systems |
| 02/14/2006 | CA2317178C Uplink demodulator scheme for a processing satellite |
| 02/09/2006 | WO2006013062A1 Method and system of detecting, monitoring and defining parameters for flying or stationary objects in airspace and outer space |
| 02/09/2006 | WO2005113337A3 Electromagnetic device for generating a force and a torque in order to position a body |
| 02/09/2006 | US20060027709 Apparatus comprising of propulsion system |
| 02/09/2006 | US20060027708 Method and system for CMG array singularity avoidance |
| 02/09/2006 | US20060027700 Lightning strike mitigation system |
| 02/08/2006 | EP1227977B1 Method and apparatus for minimizing the transmission of acoustic vibrations to a payload |
| 02/07/2006 | US6995705 System and method for doppler track correlation for debris tracking |
| 02/07/2006 | US6994296 Apparatus and method for maneuvering objects in low/zero gravity environments |
| 02/07/2006 | US6994153 Heat discharger suitable for application to heat pipes |
| 02/02/2006 | US20060022091 Method and system for optimizing torque in a cmg array |
| 02/01/2006 | EP1476356B1 Method and system for balancing thrust demands |
| 01/26/2006 | US20060016935 Modular spacecraft design architecture |
| 01/26/2006 | US20060016934 Method for deploying multiple spacecraft |
| 01/25/2006 | EP1619123A2 Staged emitter-attractor ion drive |
| 01/25/2006 | EP1618039A1 Momentum stabilized launch vehicle upper stage |
| 01/24/2006 | US6990396 Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector |
| 01/19/2006 | WO2006005833A1 Method for detecting complete draining of a propellant tank and for propellant management onboard a satellite |
| 01/19/2006 | WO2005095891A8 Gyroscope apparatus |
| 01/19/2006 | US20060011783 Method for controlling the attitude of an satellites in elliptic orbits using solar radiation pressure |
| 01/18/2006 | EP1616790A1 Method for attitude control of satellites in elliptic orbits using solar radiation pressure |
| 01/18/2006 | EP1615821A1 Method and receiver for the simultaneous detection and evaluation of at least two electromagnetic signals |
| 01/18/2006 | EP1025617B1 Integrated circuit microsatellite |
| 01/12/2006 | US20060006289 Reversable space plane |
| 01/11/2006 | CN1718510A Driving and steering integrated wheel of moon craft |
| 01/11/2006 | CN1718509A Six wheel symmetrical active suspension mechanism of moon craft |
| 01/10/2006 | US6983914 Deployable solar array assembly |
| 01/10/2006 | CA2265448C Delay compensated doppler radar altimeter |
| 01/05/2006 | US20060000514 Fluidic diverter valve with a non-spherical shuttle element |
| 01/05/2006 | DE102004026625A1 Wing or tail element with leading edges and trailing edges for aircraft with flying speeds in supersonic range has at least one end face contour extending in longitudinal direction constructed in meander form |
| 01/04/2006 | EP1612141A1 Device for the releasable holding of parts |
| 01/03/2006 | US6983198 Onboard satellite processing to mitigate data recorder limits |
| 01/03/2006 | US6981816 Apparatus for releasably interconnecting structural components having a rotational symmetry |
| 01/03/2006 | US6981364 Combine engine for single-stage spacecraft |
| 12/29/2005 | WO2005123507A1 Ultrahigh altitude sun synchronous orbit satellite system |
| 12/29/2005 | US20050284986 Orbital debris shield |
| 12/29/2005 | DE202005013162U1 Space shuttle heat shield consisting of an outer layer of reinforced carbon-carbon tiles, over a vacuum void and bonding layer |
| 12/28/2005 | EP1608863A2 Unitized hybrid rocket system |
| 12/28/2005 | EP1608555A2 Winged spacecraft |
| 12/27/2005 | US6980893 Phase recovery filtering techniques for SCP throughput shortage |
| 12/27/2005 | US6979986 Switch shunt regulator and power supply arrangement using same for spacecraft applications |
| 12/27/2005 | US6978966 Reflector deployment error estimation |
| 12/22/2005 | US20050279890 Latching separation system |
| 12/22/2005 | US20050279889 Variable wing spacecraft |
| 12/21/2005 | EP1606644A1 Method and device for assigning weighting coefficients for performing attitude calculations with a star sensor |
| 12/21/2005 | EP1606164A1 Remotely releasable support strut |
| 12/20/2005 | CA2227549C White pigments stabilised against uv radiation by an oxidising agent |
| 12/15/2005 | WO2005118395A1 Method for forming an on-orbit navigation satellite system |
| 12/15/2005 | WO2005118394A1 Propulsion unit for spacecraft, servicing system for providing in-space service operations, and modular spacecraft |
| 12/15/2005 | US20050274849 Highly-integrated low-mass solar sail |
| 12/15/2005 | DE10050715B4 Solarwärme-Rakete Solar thermal rocket |
| 12/14/2005 | EP1604110A2 Drive device pertaining to a space missile and method for controlling the position of a space missile comprising one such drive device |