| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 05/16/2002 | WO2002020346A3 An asymmetric gravitational wave propulsion system |
| 05/16/2002 | US20020056791 Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material |
| 05/16/2002 | US20020056790 Micro louvers for cooling satellites |
| 05/16/2002 | US20020056248 Foldable member |
| 05/16/2002 | CA2415313A1 Method and system for densifying cryogenic propellants |
| 05/15/2002 | CN1084698C Elastically deformable antenna reflector for spacecraft, and spacecraft including such reflector |
| 05/14/2002 | US6389336 Overhead system of inclined eccentric geosynchronous orbiting satellites |
| 05/14/2002 | US6388427 Battery temperature derivative charging |
| 05/14/2002 | US6386484 Failure resistant multiline tether |
| 05/10/2002 | WO2002036429A1 Inflatable structure, array antenna having inflatable structure, and inflatable structure unfolding method |
| 05/10/2002 | WO2001055663A3 Separation system for missile payload fairings |
| 05/09/2002 | US20020053627 Satellite system and method of deploying same |
| 05/08/2002 | EP1202905A2 Reusable, separable, structural connector assembly |
| 05/08/2002 | DE10052422A1 Familie modularer Raketentriebwerke Family of modular rocket engines |
| 05/07/2002 | US6385512 System and method of a ballistic capture transfer to L4, L5 |
| 05/07/2002 | US6382565 Satellite spin reorientation using a single degree of freedom momentum storage device |
| 05/02/2002 | US20020050340 Passive cooler comprising dual elliptically-based cones |
| 05/02/2002 | EP1202034A1 Passive cooler with double cone with elliptic base |
| 05/01/2002 | CN1083788C Low earth orbit payload launch system |
| 05/01/2002 | CN1083787C Method for launching satellites by using highly eccentric orbits and atmospheric braking |
| 05/01/2002 | CN1083786C Method and system for putting space vehicle into orbit, uisng thrusters of high specific impulse |
| 04/30/2002 | US6381520 Sun seeking solar array control system and method |
| 04/30/2002 | US6380526 Employing booster trajectory in a payload inertial measurement unit |
| 04/30/2002 | US6378810 Satellite having a solar generator on a deployable arm, and method of bringing such a satellite on station |
| 04/30/2002 | US6378809 AFT deployable thermal radiators for spacecraft |
| 04/30/2002 | US6378292 MEMS microthruster array |
| 04/25/2002 | US20020047673 Propulsion device and method of generating shock waves |
| 04/25/2002 | US20020047072 Lift multiplying device for aircraft |
| 04/24/2002 | EP1199250A1 Improvements applied to geostationary satellites |
| 04/24/2002 | EP1198864A1 System comprising a satellite with radiofrequency antenna |
| 04/24/2002 | CN1083553C Three-dimensionally reinforced ablative/insulative composite |
| 04/24/2002 | CN1083374C Satellite communication system at an inclined orbit |
| 04/23/2002 | US6377352 Angular rate and reaction torque assembly |
| 04/23/2002 | US6375125 Hybrid composites for oxygen propulsion systems |
| 04/23/2002 | US6374618 Cryogenic fluid supply from supercritical storage system |
| 04/23/2002 | US6374565 Foldable member |
| 04/18/2002 | WO2002031918A1 Radiation reflector |
| 04/18/2002 | WO2002030748A1 System and method for modifying and controlling trajectories of spacecrafts during space or air navigation and to modify trajectories of inert bodies moving in space |
| 04/18/2002 | WO2001070573A3 Passive, multi-axis, highly damped, shock isolation mounts |
| 04/18/2002 | DE10059914A1 Vorrichtung zum Bergen von Raumflugkörpern Apparatus for recovering spacecraft |
| 04/18/2002 | DE10049990A1 Displacement force device e.g. for spacecraft propulsion drive, uses conversion of impulse force of gas flow into displacement force |
| 04/18/2002 | DE10007372C2 Thermalschutzsystem für Raumfahrzeuge Thermal protection system for spacecraft |
| 04/17/2002 | EP1196326A1 Method and device for integrating satellites on a launcher |
| 04/16/2002 | US6373449 Hybrid inflatable antenna |
| 04/16/2002 | US6371413 Artificial satellite equipped with generators of magnetic and aerodynamic moments and control process for such a satellite |
| 04/16/2002 | US6371412 Method and apparatus for reducing acoustic coupling |
| 04/16/2002 | US6371406 Progressive 3-axis multi-variable propulsion vectoring aerial and spacecraft vehicle |
| 04/11/2002 | WO2002029268A2 Flywheel |
| 04/11/2002 | WO2001076944A3 Structure including a plurality of cells of cured resinous material |
| 04/11/2002 | US20020042669 Offline apparatus for detecting attitude of artificial satellite in wide-band and method thereof |
| 04/11/2002 | US20020040951 Asonic aerospike engine |
| 04/11/2002 | US20020040950 System and method for spacecraft attitude control |
| 04/11/2002 | US20020040726 Roll-out solar generator with a roll-out array structure and method of using same |
| 04/10/2002 | CN1343869A Impulse administration plan of solid propellant gas generator having high quality flow regulating rate |
| 04/09/2002 | US6367739 Compound exhaust system |
| 04/09/2002 | US6367243 Atomic-based combined cycle propulsion system and method |
| 04/09/2002 | CA2077125C Self-supporting convex cover for spacecraft |
| 04/04/2002 | WO2002027730A1 Method and device for heating gas from a thin layer of nuclear fuel, and space engine using such method |
| 04/04/2002 | US20020038840 Satellite, satellite control method and satellite communication system |
| 04/04/2002 | DE10104026A1 System in system method for space ship creates permanent vertically-directed acceleration by using ball-shaped object held by ball-bearings |
| 04/03/2002 | EP1193888A1 Slice based architecture for a multifunction radio |
| 04/03/2002 | EP1193719A1 Method and device for heating gas from a thin layer of nuclear fuel, and space engine using such method |
| 04/03/2002 | EP1193406A2 Remote activation mechanism for equipment regulated deployment or release |
| 04/03/2002 | EP1193176A2 A method and apparatus for rate integration supplement for attitude referencing with quaternion differencing |
| 04/03/2002 | EP1192380A1 Service valve and use of same in reaction control system |
| 04/03/2002 | CN1342619A Glass for sealed cabin of space environment or polar region |
| 04/02/2002 | US6366255 Main reflector and subreflector deployment and storage systems |
| 04/02/2002 | US6365822 Power system having a radioisotope heat source |
| 04/02/2002 | US6364252 Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair |
| 03/28/2002 | WO2001091310A3 Multi-node point-to-point satellite communication system employing multiple geo satellites |
| 03/28/2002 | WO2001020966A3 Elastomerized phenolic resin ablative insulation for rocket motors |
| 03/28/2002 | US20020036766 Satellite constellation for measuring atmospheric wind speeds using doppler lidar |
| 03/28/2002 | US20020036251 Inertial sensor for the mounting and checking of an inertial reference in a satellite |
| 03/28/2002 | US20020036250 Method for maintaining the position of geostationary satellites |
| 03/28/2002 | DE10043631A1 Linearbetätigungsvorrichtung, insbesondere für Raumfahrzeuge und Solargenerator-Entfaltsysteme sowie Solargenerator-Entfaltsystem Linear actuator, especially for spacecraft and solar generator Entfaltsysteme and solar generator deployment system |
| 03/28/2002 | DE10043249A1 Ausfahrbare Trägerstruktur aus verformbaren Rohrelementen Extendable support structure of malleable elements |
| 03/27/2002 | EP1191271A2 Remote activation mechanism for equipment hold down and release |
| 03/27/2002 | EP1190948A2 Spacecraft recovery device |
| 03/27/2002 | EP1189847A2 Photocatalytic coatings on optical solar reflectors to decompose organic contaminants |
| 03/27/2002 | EP1189711A1 Manufacturing a dome from an undersized blank |
| 03/27/2002 | EP1040274B1 Pump with positive displacement |
| 03/27/2002 | CN1341536A Spin-stabilized film reflector and its application in space |
| 03/26/2002 | US6362464 System for stellar inertial attitude determination |
| 03/26/2002 | US6361869 Arc discharging in components exposed to charge flux and coated with polymetallocene |
| 03/26/2002 | US6361312 High temperature materials processing furnace |
| 03/26/2002 | US6361055 Cryogenic composite tank seals |
| 03/26/2002 | US6361018 Coaxial valve with electric actuating drive |
| 03/26/2002 | US6360996 Steering control for skewed scissors pair CMG clusters |
| 03/26/2002 | US6360995 Docking system & method for space travel vehicle |
| 03/26/2002 | US6360994 Configurable space launch system |
| 03/26/2002 | US6360993 Expendable launch vehicle |
| 03/21/2002 | WO2002022443A1 Device and method for a spacecraft |
| 03/21/2002 | US20020035419 Autonomous navigation, guidance and control using LDRI |
| 03/21/2002 | US20020033796 Pointing device and an onboard pointing system |
| 03/21/2002 | US20020032992 Extendable support structure of deformable tube elements |
| 03/20/2002 | EP1189329A2 Space photovoltaic power generation method and system |
| 03/20/2002 | EP1189328A2 Space photovoltaic power generation system, power satellite, and electric power producing ground station |
| 03/20/2002 | EP1189327A2 Method of and system for receiving microwave |
| 03/20/2002 | EP1189301A2 Main reflector and subreflector deployment and storage systems |
| 03/20/2002 | EP1188731A2 Coating having high resistance to heat and oxidation and multi-coated material having high resistance to heat and oxidation |