| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 02/22/2005 | US6859769 Method and apparatus for creating elements and systems for description of position and motion of bodies in three-dimensional space to support orbital maneuver analysis |
| 02/22/2005 | US6859170 Extended kalman filter for autonomous satellite navigation system |
| 02/22/2005 | US6857602 Environmental control system and method of using the same |
| 02/22/2005 | US6857269 Capillary two-phase thermodynamic power conversion cycle system |
| 02/17/2005 | WO2005015015A1 Method for production and conversion of energy into mechanical motion |
| 02/17/2005 | WO2004051188A3 Torque induced propulsion system |
| 02/17/2005 | US20050038602 Terrestrial environment observation satellites |
| 02/17/2005 | US20050034447 Polyoxymethylene as structural support member and propellant |
| 02/17/2005 | DE10331740A1 Missile in form of electrically driven airship or spaceship, has three axially symmetrical and relatively moving components, i.e. central thrust collar, ring shaped body and sphere shaped crew cabin |
| 02/17/2005 | DE10031542B4 Inertialsensor zur Lagerung und Kontrolle einer Inertialreferenz in einem Satelliten Inertial sensor for storage and control of inertial reference in a satellite |
| 02/15/2005 | US6854510 Spacecraft radiator system and method using cross-coupled deployable thermal radiators |
| 02/10/2005 | WO2004098994A3 Attitude determination and control system for a solar sail spacecraft |
| 02/10/2005 | US20050029405 Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits |
| 02/10/2005 | US20050029397 Flying saucer |
| 02/08/2005 | US6852271 Flexible insulation blanket having secondarily bonded ceramic matrix composite layer |
| 02/08/2005 | US6851651 Constellation of spacecraft, and broadcasting method using said constellation |
| 02/03/2005 | WO2003071308A8 Constellation of spacecraft, and broadcasting method using said constellation |
| 02/03/2005 | US20050027496 Method for computer-assisted determination of an optimum-fuel control of nozzles |
| 02/03/2005 | US20050027407 Autonomous manoeuring for spinning spacecraft |
| 02/03/2005 | US20050023415 Spacecraft with extensible radiators |
| 02/03/2005 | US20050023052 Vehicle having an articulated suspension and method of using same |
| 02/03/2005 | US20050022465 Flexible, deployment rate damped hinge |
| 02/02/2005 | CN1572655A Power conditioning architecture for spacecraft |
| 02/01/2005 | US6850875 Method and apparatus for determining obscuration of sensors that are mounted on a spacecraft |
| 02/01/2005 | US6848796 Radiation reflector |
| 01/27/2005 | US20050018198 Integrated reaction wheel assembly and fiber optic gyro |
| 01/27/2005 | US20050017132 Asonic aerospike engine |
| 01/27/2005 | US20050016157 Combined engine for single-stage spacecraft |
| 01/27/2005 | DE202004018418U1 Schweißzange Welding gun |
| 01/26/2005 | EP1501132A2 Solar array for deployment in two dimensions |
| 01/26/2005 | EP1500880A2 A transpiration cooling system |
| 01/26/2005 | EP1500590A1 Restrainer rod release device for a deployable structure |
| 01/26/2005 | CN1569565A Convenient and feasible project for space shuttle used in civil aviation |
| 01/25/2005 | US6847867 Satellite communication with low probability of detection |
| 01/25/2005 | US6845952 Flywheel prognostic health and fault management system and method |
| 01/25/2005 | US6845951 Method of controlling pointing for a flexible structure |
| 01/25/2005 | US6845950 System for high efficiency spacecraft orbit transfer |
| 01/25/2005 | US6845949 System and methods for integrating a payload with a launch vehicle |
| 01/20/2005 | WO2005005255A1 Aerospace vehicle with separate propellant reservoir or energy source |
| 01/20/2005 | WO2004101360A3 Momentum control system and method |
| 01/19/2005 | CN1568527A Switchable magnetic device |
| 01/19/2005 | CN1566631A Electromagnetic radiation device |
| 01/19/2005 | CN1185139C Miniature colloid impeller and making method thereof |
| 01/18/2005 | US6845303 Micro-satellite and satellite formation for inverse and distributed proximity operations |
| 01/18/2005 | US6844844 System comprising a satellite with radiofrequency antenna |
| 01/18/2005 | US6844714 Satellite charge monitor |
| 01/18/2005 | US6844703 Battery cell balancing system |
| 01/18/2005 | US6844057 Method for secondarily bonding a ceramic matrix composite layer to a flexible insulation blanket and an insulation blanket produced thereby |
| 01/18/2005 | US6843462 Manufacturing apparatus of fiber reinforced composite member |
| 01/18/2005 | US6843446 Apparatus and methods for in-space satellite operations |
| 01/18/2005 | US6843029 Apparatus including a boom to be compressed and rolled up |
| 01/18/2005 | CA2344125C Working robot |
| 01/13/2005 | WO2005003579A1 Piezodynamic preload adjustment system |
| 01/13/2005 | WO2005002967A1 Piezodynamic vibration damping system |
| 01/13/2005 | US20050010337 Relative attitude estimator for multi-payload attitude determination |
| 01/13/2005 | DE10353651A1 Operating method for discus shaped vertically starting/landing reusable single-stage space flight vehicle, involves use of cryogenic gas, e.g. liquid methane, to operate turbines of ramjet burner |
| 01/12/2005 | EP1495964A1 Heat dissipation device with double conduction for spacecraft |
| 01/12/2005 | EP1494919A1 Virtual reaction wheel array using control moment gyros |
| 01/12/2005 | EP1127004B1 Method and apparatus for determining the yaw angle of a satellite |
| 01/11/2005 | US6840481 Adjustable multipoint docking system |
| 01/11/2005 | US6840275 Variable-gravity anti-vortex and vapor-ingestion-suppression device |
| 01/06/2005 | WO2005000574A2 Positive pressure hot bonder |
| 01/06/2005 | WO2004071869B1 Device for controlling the attitude of a satellite by means of gyroscopic actuators |
| 01/06/2005 | US20050001102 System and method for attitude control and station keeping |
| 01/06/2005 | US20050001101 Surface optical reflector, for a space craft such as a geostationary satellite |
| 01/05/2005 | EP1493788A1 Silicone-cork ablative material |
| 01/05/2005 | EP1492706A1 Spacecraft, method for building such a spacecraft, and adaptor to be used in such a spacecraft |
| 01/05/2005 | EP1492705A2 Satellite energy and attitude control system |
| 01/05/2005 | CN1182985C Hybrid electric vehicle with traction motor drive allocated according to battery charge state |
| 01/04/2005 | US6837464 Lox-compatible composite tank for aerospace applications |
| 12/30/2004 | US20040263024 Piezodynamic preload adjustment system |
| 12/30/2004 | US20040262457 Inflatable Parachute for Decelerating an Object Entering the Earth Atmosphere from the Outer Space |
| 12/30/2004 | US20040262440 Mass trim mechanism |
| 12/30/2004 | US20040261569 Piezodynamic vibration damping system |
| 12/30/2004 | DE202004014122U1 Schwimmende Startanlage für einen Raumflugkörper Floating starting system for a spacecraft |
| 12/29/2004 | WO2004113170A1 Satellite launch apparatus |
| 12/29/2004 | WO2004085252A3 Unitized hybrid rocket system |
| 12/29/2004 | EP1490654A1 Inertial control and measurement system |
| 12/29/2004 | EP1179132B1 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 12/29/2004 | EP1179131B1 An apparatus for controlling the flow separation line of rocket nozzles |
| 12/29/2004 | EP0991571B1 Quick installation-removal thermal insulation blanket for space craft |
| 12/29/2004 | EP0991570B1 Quick installation-removal thermal insulation blanket for spacecraft |
| 12/28/2004 | US6835262 Positive pressure hot bonder |
| 12/28/2004 | US6834841 Method and system for decoupling structural modes to provide consistent control system performance |
| 12/28/2004 | US6834561 Radially actuated control moment gyroscope |
| 12/23/2004 | WO2004033296A3 System and method for increasing the roll offset operating range for a spacecraft |
| 12/23/2004 | US20040258900 Multi-layer ceramic composite material with a thermal-protective effect |
| 12/23/2004 | US20040256045 Positive pressure hot bonder |
| 12/22/2004 | EP1487700A1 Inertial reference system for a spacecraft |
| 12/22/2004 | EP1187979B1 Rocket thrust chamber |
| 12/16/2004 | WO2004108532A1 Remotely releasable support strut |
| 12/16/2004 | WO2004108531A1 Surface temperature control system |
| 12/16/2004 | WO2004022867B1 Stiffener reinforced foldable member |
| 12/16/2004 | US20040251885 Switch shunt regulator and power supply arrangement using same for spacecraft applications |
| 12/16/2004 | US20040251689 Space colony factory unit with gravity generator |
| 12/16/2004 | US20040250503 Multi-purpose beam |
| 12/15/2004 | EP1486845A1 Switching shunt regulator and power supply arrangement using same, in particular for spacecraft applications |
| 12/15/2004 | EP1485732A2 Constellation of spacecraft, and broadcasting method using said constellation |
| 12/15/2004 | EP1485727A1 Method and arrangements for the transmission of pseudolite trajectories within navigation data of a satellite navigation system |
| 12/15/2004 | EP1485292A1 Control moment gyro for attitude control of a spacecraft |