Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64G - Cosmonautics; Vehicles or equipment therefor › B64G 1 - Cosmonautic vehicles
Patents for B64G 1 - Cosmonautic vehicles (11,089)
05/2003
05/27/2003US6571156 Spacecraft power acquisition procedure and method for wing-deployed configuration
05/27/2003US6570591 Visual syntax builder for space vehicle control
05/27/2003US6568640 Inflatable satellite design
05/27/2003US6568639 Autonomous orbit transfer vehicle
05/27/2003US6568638 Modular spacecraft structure
05/27/2003US6568291 Shaftless gyrostabilizer
05/22/2003WO2003042632A1 Gyroscopic actuator
05/22/2003WO2003042038A1 Surface optical reflector, for space craft such as a geostationary satellite
05/22/2003WO2000078610A3 Fly back booster
05/22/2003US20030096894 Method of constructing insulated metal dome structure for a rocket motor
05/22/2003US20030096609 Method and apparatus for orbit determination
05/22/2003US20030094236 Method of constructing insulated metal dome structure for a rocket motor
05/22/2003US20030093987 Integrated tankage for propulsion vehicles and the like
05/21/2003EP1312997A1 Low earth orbit satellite attitude and stabilisation control method using coupling with earth's magnetic field
05/21/2003EP1312546A1 Method for generating a divergence between central time and peripheral time in a rotating system applicable to a spatial vehicle
05/21/2003EP1311428A1 Employing booster trajectory in a payload inertial measurement unit
05/20/2003US6567712 Method for determining the co-ordinates of a satellite
05/20/2003US6567040 Offset pointing in de-yawed phased-array spacecraft antenna
05/20/2003US6566640 System and method for autonomous correction of star tracker high spatial frequency (HSF) error
05/20/2003US6566633 Thermal control apparatus and method for thermally controlling a plurality of objects within a predetermined temperature range
05/20/2003US6565044 Combination solar sail and electrodynamic tether propulsion system
05/20/2003US6565043 Redundant system for satellite inclination control with electric thrusters
05/15/2003US20030093194 Attitude determination system and method with outer-loop gyro scale-factor non-linearity calibration
05/15/2003US20030089821 Payload delivery system
05/15/2003US20030089484 Electrostatic switched radiator for space based thermal control
05/14/2003EP1234117B1 Shockproof mechanism, in particular for use in space sector
05/14/2003CN1418290A Plasma accelerator arrangement
05/14/2003CN1108669C Hybrid constellation satellite communication systems and methods with efficient signaling and control
05/13/2003US6561462 Spacecraft power/sun aquistion algorithm using slit sun sensors
05/13/2003US6561461 Orbit transfer vehicle with support services
05/13/2003US6560942 Open lattice, foldable, self deployable structure
05/13/2003CA2199436C Earth based spacecraft orbit and attitude control using a look-ahead thruster selection logic and magnetic torquers
05/08/2003US20030085323 Deployable radiator with flexible line loop
05/07/2003EP1308813A1 Method of attitude control of a low earth orbit satellite
05/07/2003CN1107615C System for changing rigidity and damping property of structural connecting piece
05/06/2003US6560534 Method and apparatus for distributing satellite tracking information
05/06/2003US6558785 Insulated reentry heat shield
05/06/2003US6557804 Rotating solar concentrator
05/06/2003US6557803 Crewed on-orbit, returnable, and reusable space vehicle
05/06/2003US6557802 Device for separation of a plurality of axially arranged satellites
05/02/2003EP1305211A1 Modular reaction wheel assembly to shield electronics on a satellite
05/02/2003EP1156960A4 Autonomous stratospheric airship
05/02/2003EP0939726A4 Thrust levitation
05/01/2003WO2003036404A1 Autonomous manoeuring for spinning spacecraft
05/01/2003US20030082332 Passive intermodulation free multilayer thermal blanket
05/01/2003US20030080255 Attitude control methods and systems for multiple-payload spacecraft
05/01/2003US20030080241 Air launch of payload carrying vehicle from a transport aircraft
04/2003
04/29/2003US6556165 Antenna apparatus and waveguide rotary coupler
04/29/2003US6555740 Extendible solar generator with an extendible supporting array structure
04/29/2003US6555211 Carbon composites with silicon based resin to inhibit oxidation
04/29/2003US6554936 Method of constructing insulated metal dome structure for a rocket motor
04/29/2003US6554228 Aerodynamic fairing
04/29/2003CA2404285A1 Passive intermodulation free multilayer thermal blanket
04/24/2003WO2003033349A1 Coupling for a space vessel
04/24/2003WO2002083595A3 Thermal protection system having a variable density of fibers
04/24/2003US20030076215 Inverted split-spool release devices
04/24/2003US20030075645 Energy managed electric propulsion methods and systems for stationkeeping satellites
04/23/2003CN1413294A Shockproof mechanism, in particular for use in space sector
04/23/2003CN1412083A Superhigh pressure pneumatic space aircraft
04/22/2003US6550721 Safing mode for high momentum states in body stabilized spacecraft
04/22/2003US6550720 Aerobraking orbit transfer vehicle
04/22/2003US6550209 Modular deployable antenna
04/17/2003WO2003031931A2 Method and apparatus to produce ions and nanodrops from taylor cones of volatile liquids at reduced pressures
04/17/2003WO2002103203A3 Fluid transfer system
04/17/2003US20030072666 Support apparatus for movable member and pump apparatus
04/17/2003US20030071712 Thermal-effect controlled-release mechanism
04/17/2003CA2462854A1 Method and apparatus to produce ions and nanodrops from taylor cones of volatile liquids at reduced pressures
04/16/2003EP1301396A1 Solar concentrator
04/16/2003CN1105945C Apertured nonplanar electrodes and forming methods
04/15/2003US6547476 Universal spacecraft separation node
04/15/2003US6547190 Application of carbon fiber mesh for space and airborne platform applications
04/15/2003US6547189 Inflatable vessel and method
04/15/2003US6547182 Solid rocket motor bolted thrust takeout structure
04/10/2003US20030066969 Method and apparatus to produce ions and nanodrops from taylor cones of volatile liquids at reduced pressures
04/09/2003EP1299673A2 Method and system for densifying cryogenic propellants
04/09/2003EP0932549B1 Autonomous solar torque management
04/08/2003US6545853 Alternate grounding method
04/08/2003US6544056 Temperature-controlled wire support
04/08/2003US6543725 Flexible, foldable solar generator for spacecrafts
04/08/2003US6543724 Miniature satellite design
04/08/2003US6543723 Electric orbit raising with variable thrust
04/08/2003US6543715 Aerospace system
04/03/2003WO2003027704A2 Satellite attitude adjustment for gps initialization
04/03/2003WO2003027499A2 Rotating propulsion device
04/03/2003US20030062452 Electric orbit raising with variable thrust
04/01/2003US6542820 Method and apparatus for generating and distributing satellite tracking information
04/01/2003US6541916 Method for providing discharge power to electric propulsion thrusters
04/01/2003US6539799 Rotational speed measurement device for rotating missiles
04/01/2003US6539703 Spacecraft component with microthruster actuation and operation thereof
03/2003
03/27/2003WO2003026027A2 Solar array concentrator system and method for concentrating solar energy
03/27/2003WO2003024798A1 Esd coatings for use with spacecraft
03/27/2003WO2003024797A2 Propellant utilization system
03/27/2003WO2002070345A9 Supplying space platforms with intermediate orbital docking
03/27/2003US20030058161 Satellite attitude adjustment for GPS initialization
03/27/2003US20030057354 System and method for autonomous correction of star tracker high spatial frequency (hsf) error
03/27/2003US20030057330 Solar array concentrator system and method
03/27/2003US20030057329 Application of carbon fiber mesh for space and airborne platform applications
03/27/2003US20030057328 Spacecraft having a nonuniform body shape
03/27/2003US20030057319 Propulsion device with decreased mass
03/27/2003US20030056838 Variable-gravity anti-vortex and vapor-ingestion-suppression device
1 ... 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 ... 111