Patents for B64G 1 - Cosmonautic vehicles (11,089)
10/2003
10/08/2003EP1350989A2 Temporary locking device for a rotor, especially of a fly wheel rotor with magnetic suspension for space applications
10/08/2003CN1446730A Radiation hardening shield method
10/07/2003US6631314 Propellant utilization system
10/07/2003US6629673 Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion
10/07/2003US6629672 Sun sensor alignment compensation system
10/07/2003US6629486 Resettable separation nut with a low level of induced shock
10/07/2003US6629353 Dome made of aluminum alloy; particularly intended to form the bottom of a tank; and method of manufacturing it
10/02/2003WO2003080439A1 Control moment gyro for attitude control of a spacecraft
10/02/2003US20030183727 Crewed on-orbit, returnable, and reusable space vehicle
10/02/2003US20030183726 Space cargo delivery apparatus
10/02/2003US20030183035 Device for temporarily locking a rotor, in particular a magnetically suspended rotor of an inertia wheel for space applications
10/02/2003US20030182879 Stiffener reinforced foldable member
10/02/2003US20030182878 Flat folding tube
10/01/2003EP1347916A1 A system and method for implementing a constellation of non-geostationary satellites that provides simplified satellite tracking
10/01/2003EP1211177B1 Aerospace system
10/01/2003EP1207103B1 Method for controlling an aerospace system to put a payload into an orbit
10/01/2003CN2576607Y Micro gel-propeller
09/2003
09/30/2003US6626603 Screw mounting installation and apparatus
09/30/2003US6626231 Heat transfer device
09/25/2003WO2003079044A1 Method and arrangements for the transmission of pseudolite trajectories within navigation data of a satellite navigation system
09/25/2003US20030177757 Propellant supply device
09/25/2003DE10208724C1 Verfahren zur Erfassung von durch den Aufprall von Fremdkörpern verursachten Beschädigungen an Raumfahrzeugen A method for detecting caused by the impact of foreign bodies damage to spacecraft
09/24/2003EP1346915A2 Propellant supply device
09/23/2003US6625586 Model optimization adaptive control method
09/23/2003US6623826 Passive intermodulation free multilayer thermal blanket
09/23/2003US6622971 Adapter for connecting rocket stages
09/23/2003US6622970 Method and apparatus for autonomous solar navigation
09/23/2003US6622969 Maneuver device for artificial satellite
09/23/2003US6622579 Bearing arrangement for tension forces and bearing head therefor
09/23/2003CA2065356C Capture/berthing system for spacecraft
09/18/2003WO2003077324A1 Apparatus and method for the design and manufacture of foldable integrated device array stiffeners
09/18/2003US20030173469 Combined thrust and power generator for a satellite
09/18/2003US20030173468 Electrostatic 512kV rotator and/or oscillator propulsion system
09/18/2003US20030173467 Satellite deployment structure
09/18/2003US20030173466 Spaceshuttle observatory
09/18/2003US20030173465 Spaceshuttle telescope-observatory
09/18/2003US20030173464 Spaceshuttle launched double observatory
09/18/2003US20030173463 Spaceshuttle double observatory
09/18/2003US20030173462 Spaceshuttle launched observatory
09/18/2003US20030173461 Spaceshuttle forked observatory
09/18/2003US20030172659 Method and system for densifying cryogenic propellants
09/17/2003EP1240532B1 Sun sensors using multi-pinhole overlays for detection of satellite attitude
09/16/2003US6621453 Satellite attitude adjustment for GPS initialization
09/16/2003US6619031 Multi-mode multi-propellant liquid rocket engine
09/11/2003US20030171855 Spacecraft methods and structures with enhanced attitude control that facilitates gyroscope substitutions
09/11/2003US20030170071 Positive lock quick release pin
09/11/2003US20030167763 Contingency hydraulic power unit
09/10/2003EP1064591B1 Continuous spacecraft attitude control that avoids cmg array singularities
09/09/2003US6618025 Lightweight, compactly deployable support structure with telescoping members
09/09/2003US6616104 Spacecraft configuration and attitude steering method for highly inclined orbit (HIO) communications
09/09/2003US6616092 Reusable flyback rocket booster and method for recovering same
09/09/2003US6615609 Accumulator
09/04/2003WO2003073366A1 Pattern recognition system
09/04/2003WO2003073122A1 Method for the detection of damage to spacecraft caused by the impact of foreign bodies
09/04/2003WO2003072436A1 Dynamic unbalance compensation system and method
09/04/2003US20030164429 Satellite harmonic torque estimator
09/04/2003US20030164428 Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking
09/04/2003US20030164427 ESD coatings for use with spacecraft
09/04/2003US20030164186 Apparatus and method for the design and manufacture of foldable integrated device array stiffeners
09/04/2003US20030163986 Pressure-actuated joint system
09/03/2003EP1339604A1 Device and method for connecting two parts of a craft
09/03/2003CN1120113C Payload carry and launch system
09/03/2003CN1120028C Method for playing space game and devices for realising this method
09/02/2003US6615117 Attitude determination system and method with outer-loop gyro scale-factor non-linearity calibration
09/02/2003US6612522 Flyback booster with removable rocket propulsion module
09/02/2003US6612192 Scanning apparatus and method that avoids unwanted reactions
08/2003
08/28/2003WO2003071308A2 Constellation of spacecraft, and broadcasting method using said constellation
08/28/2003WO2003070570A1 Method and system for balancing thrust demands
08/28/2003US20030160132 Dynamic unbalance compensation system and method
08/27/2003EP1338509A2 Satellite with a radiator surface
08/27/2003EP1337806A1 Ground test bench for stellar sensor
08/27/2003EP1198864B1 System comprising a satellite with radiofrequency antenna
08/27/2003CN1119522C Rocket assembly ablative materials formed from, as precursor, staple cellulose fibers, and method of insulating or thermal protecting rocket assembly with same
08/26/2003US6611683 Elliptical satellite system which emulates the characteristics of geosynchronous satellites
08/26/2003US6609683 Supporting structure for a solar sail of a satellite
08/26/2003US6609681 Method and apparatus for damping vibration
08/21/2003WO2003068600A1 Shoc isolation system for spacecraft fairing
08/21/2003WO2002053455A9 A system and method for implementing a constellation of non-geostationary satellites that provdides simplified satellite tracking
08/21/2003US20030158943 Real time data retrieving method of off-land transportation
08/21/2003US20030155468 Constellation of spacecraft, and broadcasting method using said constellation
08/21/2003US20030155003 Solar energy concentrator device for spacecraft and a solar generator panel
08/20/2003EP1335852A1 A construction and a method to be used in a carrier rocket or a satellit
08/20/2003EP1121605B1 Method and device for determining the position of communication satellites
08/19/2003US6608589 Autonomous satellite navigation system
08/19/2003US6607167 Spacecraft thermal shock suppression system
08/19/2003US6607163 Autonomous stratospheric airship
08/19/2003US6606908 Inertial sensor for the mounting and checking of an inertial reference in a satellite
08/18/2003CA2372263A1 Centrifugal thruster (ct)
08/14/2003WO2003067278A2 System and method for doppler track correlation for debris tracking
08/14/2003WO2002010535A3 Iso-truss structure
08/14/2003US20030152183 Interstellar transport vehicle engine
08/14/2003US20030150961 Load relief system for a launch vehicle
08/14/2003US20030150960 Spacecraft methods and structures with beacon-receiving field-of-view matched to beacon station window
08/14/2003US20030150959 Shock isolation system for spacecraft fairing
08/14/2003US20030150958 Miniature spacecraft
08/13/2003EP1334220A1 Material for thermally loaded substrates
08/07/2003WO2003065595A2 Virtually geostationary satellite array with optimized parameters
08/07/2003WO2003064974A1 Rotor for control moment gyroscopes and reaction wheel assemblies
08/07/2003WO2003064258A1 Apparatus for cooling components in spacecraft
08/07/2003WO2003064257A1 Rotating electromagnetic propeler with motor and method for thrust production
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