| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 02/24/2004 | US6695262 Spacecraft methods and structures for enhanced service-attitude accuracy |
| 02/24/2004 | US6695261 Shock isolation system for spacecraft fairing |
| 02/24/2004 | US6695260 Virtually geostationary satellite array |
| 02/24/2004 | US6695259 Communication system, communication receiving device and communication terminal in the system |
| 02/24/2004 | US6695256 Cryogenic propellant depletion system for a launch vehicle |
| 02/19/2004 | US20040032236 Battery cell balancing system |
| 02/19/2004 | US20040031885 In orbit space transportation & recovery system |
| 02/18/2004 | EP1389582A2 Battery cell balancing system |
| 02/18/2004 | EP1162139B1 Reusable booster for the first stage of a launcher |
| 02/18/2004 | EP0928269B1 Vehicle rotation and control mechanism |
| 02/17/2004 | US6692673 Manufacturing method of fiber reinforced composite member |
| 02/17/2004 | US6691955 Spacecraft having a momentum wheel configuration that prevents zero wheel speeds |
| 02/12/2004 | WO2004012995A1 A secondary payload satellite |
| 02/12/2004 | WO2003086860A9 Commercial space transportation system |
| 02/12/2004 | US20040027764 Thermal protection device |
| 02/12/2004 | US20040026572 Dual-mode airbreathing propulsion system |
| 02/12/2004 | US20040026571 Apparatus and methods for in-space satellite operations |
| 02/12/2004 | DE10234902A1 Flying saucer for space stations and interplanetary travel has hybrid drive with segmented solar sail construction and ion thrusters |
| 02/11/2004 | EP1388493A2 Method for the propellant-optimal regulation of a nozzle assembly |
| 02/10/2004 | US6691033 System and method for calibrating inter-star-tracker misalignments in a stellar inertial attitude determination system |
| 02/10/2004 | US6689952 Large membrane space structure and method for its deployment and expansion |
| 02/05/2004 | WO2003062565A9 Open-lattice, foldable, self-deployable structure |
| 02/05/2004 | US20040021927 Electrochromic devices |
| 02/05/2004 | US20040021040 Container cabin for orbital vehicle |
| 02/05/2004 | US20040020115 Micro gravity environmental control apparatus and micro gravity environmental control method |
| 02/05/2004 | DE10333314A1 Wegstehelement zum Fixieren von Wärmeschutzplatten Wegstehelement for fixing thermal insulation panels |
| 02/05/2004 | DE10333313A1 Wärmeschutzvorrichtung Thermal protector |
| 02/04/2004 | EP1387438A1 Remotely adjustable mesh deployable reflector |
| 02/04/2004 | EP1386838A1 Deployable antenna reflector |
| 02/04/2004 | EP1385740A1 Satellite solar generator structure comprising bracing elements between panels |
| 02/04/2004 | EP1188098B1 Momentum position control |
| 02/04/2004 | EP0741655B1 Apparatus and methods for in-space satellite operations |
| 02/03/2004 | US6685142 Three-axis position control for low-orbiting satellites |
| 02/03/2004 | US6685141 X33 aeroshell and bell nozzle rocket engine launch vehicle |
| 02/03/2004 | US6684724 Shape memory alloy step drive mechanism for providing step motion to a system |
| 02/03/2004 | US6684569 Self-closing access door |
| 01/29/2004 | US20040016852 System and methods for integrating a payload with a launch vehicle |
| 01/29/2004 | US20040016846 Launch vehicle payload carrier and related methods |
| 01/29/2004 | DE10229561A1 Optische Einrichtung für Raumfahrt-Anwendungen An optical device for space applications |
| 01/27/2004 | US6683563 System for determining precise orbit of satellite and method thereof |
| 01/27/2004 | US6682020 Unfolding joint for satellite solar generators |
| 01/27/2004 | US6682019 Minimum energy wheel configurations for energy storage and attitude control |
| 01/27/2004 | US6681649 Inertial control and measurement system |
| 01/27/2004 | CA2198046C Controlled-emission solar tabs for attitude solar sailing |
| 01/22/2004 | WO2004007287A2 Integrated inertial stellar attitude sensor |
| 01/22/2004 | US20040012865 Spin-stabilized film mirror and its application in space |
| 01/22/2004 | US20040011942 Stand-off for fixing thermal protection panels |
| 01/22/2004 | US20040011925 Method and apparatus for converting electrostatic potential energy |
| 01/22/2004 | US20040011924 Lift-providing unit for levitating a platform |
| 01/21/2004 | EP1382936A1 Apparatus and method for estimating attitude using inertial measurement equipment and program |
| 01/21/2004 | EP1381883A1 Ranging system for determining ranging information of a spacecraft |
| 01/20/2004 | US6681182 Fault detection pseudo gyro |
| 01/20/2004 | US6681159 Spacecraft methods and structures with enhanced attitude control that facilitates gyroscope substitutions |
| 01/20/2004 | US6679457 Reaction wheel system with vernier control rotor |
| 01/20/2004 | US6679456 Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material |
| 01/20/2004 | US6679455 Pointing device and an onboard pointing system |
| 01/20/2004 | CA2200260C Speed regulator mechanism and mechanical motor for applications in thermal vacuum on satellites |
| 01/15/2004 | WO2004005747A2 Method and system for decoupling structural modes to provide consistent control system performance |
| 01/15/2004 | WO2004005645A1 Foldable member |
| 01/15/2004 | WO2004005134A1 Multi-function reaction wheel assemblies for controlling spacecraft attitude |
| 01/15/2004 | WO2004005133A1 Reaction wheel desaturation apparatus |
| 01/15/2004 | WO2004005019A1 Product and method for producing a non-woven fabric by means of hydrodynamic needling |
| 01/15/2004 | US20040010355 Multi-function reaction wheel assemblies for controlling spacecraft attitude |
| 01/15/2004 | US20040008137 Correlating single continuous wave radar space object observation for initial orbit determination |
| 01/15/2004 | US20040007123 Hermetically sealed actuator |
| 01/15/2004 | DE10233991A1 Produkt und Verfahren zur Herstellung eines Vliesstoffes mittels hydrodynamischer Vernadelung Product and process for producing a nonwoven fabric by means of hydrodynamic needling |
| 01/15/2004 | DE10230350A1 Raumfahrzeug mit einer Einrichtung zur Lageregelung Space vehicle having a device for position control |
| 01/15/2004 | DE10230349A1 Raumfahrzeug mit einer Einrichtung zur Wärmeregelung Space vehicle having a device for thermal control |
| 01/15/2004 | DE10224475A1 Diverse Modifikationen der elektromagnetischen Spiralleitereinheiten des Schwebemobil-Auftriebssystemes Various modifications of the electromagnetic coil conductor units of the floating mobile lift system |
| 01/14/2004 | EP1380853A2 Ranging system for determining ranging information of a spacecraft |
| 01/14/2004 | EP1107852B1 Moment control unit for spacecraft attitude control |
| 01/13/2004 | US6678519 Elliptical satellite system which emulates the characteristics of geosynchronous satellites |
| 01/13/2004 | US6677884 Satellite configuration for interferometric and/or tomographic remote sensing by means of synthetic aperture radar (SAR) |
| 01/13/2004 | US6676087 Spacecraft methods and structures with beacon-receiving field-of-view matched to beacon station window |
| 01/13/2004 | US6676077 High temperature resistant airfoil apparatus for a hypersonic space vehicle |
| 01/13/2004 | US6675571 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 01/08/2004 | US20040004161 Method and system for decoupling structural modes to provide consistent control system performance |
| 01/08/2004 | DE10321333A1 Zusammengesetzte Konstruktion zum Abschluß einer Nutzlast in den Raum Composite construction for completion of a payload into space |
| 01/08/2004 | DE10226535A1 Dreiachsige Lagebestimmung eines Satelliten durch zeitliche Propagation von zweiachsigen Sensor-Messwerten Three axis orientation of a satellite by temporal propagation of two-axis sensor metrics |
| 01/08/2004 | DE10221465A1 Schwebemobil - Auftriebssystem mit zweiarmigen Lichtwellenleiter - Spiralen Floating mobile - lift system with two-armed Fiber Optics - Spirals |
| 01/06/2004 | US6675068 Working robot |
| 01/06/2004 | US6673402 Fiber-reinforced ceramics in spacecrafts and aerodynes |
| 01/06/2004 | US6672544 Satellite harmonic torque estimator |
| 01/06/2004 | US6672542 Method and system for controlling the eccentricity of a near-circular orbit |
| 01/06/2004 | US6672539 Power generation system |
| 01/02/2004 | EP1373071A1 Solar panel with electrical terminals distributed across the surface thereof |
| 01/01/2004 | US20040000134 Pulse detonation engine having an aerodynamic valve |
| 12/31/2003 | WO2004002201A1 A plasma beam generator |
| 12/31/2003 | WO2004000647A1 Apparatus for supplying energy to the environment |
| 12/31/2003 | WO2003084813A3 Method of using dwell times in intermediate orbits to optimise orbital transfers and method and apparatus for satellite repair |
| 12/31/2003 | CN1464934A Iso-truss structure |
| 12/30/2003 | US6669148 Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking |
| 12/30/2003 | US6669147 Deployable radiator for a space vehicle |
| 12/30/2003 | US6668543 Rocket propulsion unit with separation of inner and outer casing and method of making same |
| 12/30/2003 | US6668441 Screw mounting installation method |
| 12/25/2003 | US20030234318 Unbalanced gyroscopic apparatus for producing unidirectional thrust |
| 12/24/2003 | WO2003106264A1 Cooling device for space craft |
| 12/24/2003 | WO2003071308A3 Constellation of spacecraft, and broadcasting method using said constellation |
| 12/23/2003 | US6666410 Load relief system for a launch vehicle |
| 12/23/2003 | US6666409 Crewed on-orbit, returnable, and reusable space vehicle |