Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64G - Cosmonautics; Vehicles or equipment therefor › B64G 1 - Cosmonautic vehicles
Patents for B64G 1 - Cosmonautic vehicles (11,089)
03/2003
03/26/2003EP1295170A1 Electrochromic devices
03/25/2003US6538796 MEMS device for spacecraft thermal control applications
03/25/2003US6537379 Photocatalytic coating and method for cleaning spacecraft surfaces
03/25/2003US6536713 Method of controlling or stabilizing the attitude of a vehicle in space
03/25/2003US6536712 Inflatable satellite
03/25/2003US6536090 Method for making a cryogenic tank joint
03/20/2003WO2002103199A3 Method and apparatus for ignition detection
03/20/2003US20030052232 Space transportation system
03/20/2003US20030052231 Modular RTM spacecraft bus structure
03/20/2003US20030052223 Balloon
03/20/2003US20030051857 Heat transfer device
03/20/2003DE20216977U1 Sport apparatus for astronauts enabling them to exercise in the weightless environment of outer space
03/20/2003DE20216976U1 Movement stabilizer for astronauts to enable movement and sport in the weightless environment of outer space
03/20/2003DE20216975U1 Shoes or boots for astronauts to enable movement and sport in the weightless environment of outer space
03/20/2003DE20216973U1 Gyroscopic device to generate resisting force for arm exercise for astronauts in space
03/20/2003DE20216972U1 Outer space stabilizer for astronauts to enable astronauts to exercise in a weightless environment
03/20/2003DE20216971U1 Movement stabilizer for astronauts for movement in the weightless environment of outer space
03/19/2003EP1293429A1 Multilayered hypervelocity impact shield for spacecraft
03/19/2003EP1293428A1 Heat exchanger
03/18/2003US6535801 Method and apparatus for accurately determining the position of satellites in geosynchronous orbits
03/18/2003US6535799 Dynamic technique for using corrective actions on vehicles undergoing excessive turns
03/18/2003US6534887 Microwheel
03/18/2003US6533221 Device for supporting a payload in a launch vehicle of said payload
03/18/2003US6532750 Method and system for densifying cryogenic propellants
03/13/2003US20030048053 Plasma accelerator arrangement
03/12/2003CN1401542A Miniature colloid impeller and making method thereof
03/11/2003US6530718 Connector assembly
03/11/2003US6530543 Hypersonic and orbital vehicles system
03/11/2003US6530213 Method and apparatus for ignition detection
03/11/2003US6530212 Laser plasma thruster
03/06/2003WO2003019583A1 Switchable magnetic device
03/06/2003US20030042369 Autonomous orbit transfer vehicle
03/06/2003US20030042368 Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material
03/06/2003US20030042367 Crewed on-orbit, returnable, and resuable space vehicle
03/06/2003US20030041548 Deployable truss beam with orthogonally-hinged folding diagonals
03/05/2003EP1288760A1 Method for autonomously controlling the orbit of a satellite and autonomously controlled orbiting satellite
03/05/2003EP0930994B1 Rocket launching system employing thermal-acoustic detection for rocket ignition
03/04/2003US6528719 Space photovoltaic power generation method and system
03/04/2003US6528716 Solar concentrator
03/04/2003US6527221 Shock wave modification method, apparatus, and system
03/04/2003US6527007 Fluid transfer system
02/2003
02/27/2003WO2002097829A8 Charge-dissipating, white thermal control film, and structures utilizing the thermal control film
02/27/2003WO2002058992A3 Miniature attitude sensing suite
02/27/2003US20030040273 Sub-orbital, high altitude communications system
02/26/2003EP1286038A1 Autonomous working gas supply system, use of such a system to pressurize a container, laucher stage including such a system
02/26/2003EP1068447B1 Device for controlling the relative rotation between two articulated elements and unfolding structure, in particular for space vehicle, using at least such a device
02/25/2003US6525920 Electrically and mechanically redundant release mechanism
02/25/2003US6523786 Apparatus for determining attitude of artificial satellite
02/25/2003US6523785 Reaction wheel desaturation apparatus
02/25/2003US6523784 Arrangement for recovering spacecraft
02/25/2003US6523783 Underway replenishment system for space vehicles
02/25/2003US6523782 Centrifugal sleeping section for a space craft
02/25/2003US6523338 Plasma accelerator arrangement
02/20/2003US20030034597 Shock filtering apparatus
02/20/2003US20030034422 Method for limiting interference between satellite communications systems
02/20/2003US20030033797 Description of methods to increase propellant throughput in a micro pulsed plasma thruster
02/19/2003CN1397725A Pressure actuating joint system
02/18/2003CA2091613C Method and device for detecting the relative positions and trajectories of two space vehicles
02/13/2003WO2003012804A1 Apparatus for control of uniform gravity utilizing superconducting magnet
02/13/2003US20030031505 Unfolding joint for satellite solar generators
02/13/2003US20030029970 Spacecraft methods and structures for acquiring and determining power-safe attitudes
02/13/2003US20030029969 System and method for orbiting spacecraft servicing
02/13/2003US20030029968 Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith
02/13/2003US20030029162 Propulsion module
02/13/2003DE10147144C1 Recovery method for ejected space rocket stage uses aircraft for attaching towing line to rocket stage in glider flight mode
02/12/2003EP1283168A2 Aerobraking orbit transfer vehicle
02/12/2003EP1283167A2 Orbit transfer vehicle with support services
02/12/2003EP1283162A1 Balloon
02/11/2003US6519084 Telescope and movement control device
02/11/2003US6518495 High-voltage device with a casing and protected against mobile electrical charges, and satellite equipped with the device
02/11/2003US6517029 Friction and stiction compensation for spacecraft attitude control
02/11/2003US6516604 Micro-colloid thruster system
02/06/2003US20030025042 Solar wing and tether mechanisms for asteroid uncooperative docking and asteroid orbit adjustments
02/06/2003US20030025041 Satellite communications system
02/06/2003US20030025040 Thermal protection structure
02/06/2003US20030025037 Reusable module for the storage, transportation, and supply of multiple propellants in a space environment
02/06/2003DE10130623C1 Verfahren zur Bestimmung der Zustandsgrößen eines starren Körpers im Raum mittels eines Videometers Method for determining the state variables of a rigid body in space by means of a video meter
02/05/2003CN1101073C Magnetically mounted position-stabilised flywheel
02/05/2003CN1100702C Aerodynamically actuated magnetic ascent vent cover
02/04/2003US6515221 Modular reaction wheel assembly to shield electronics on a satellite
02/04/2003US6513760 Logistics module system and method
02/04/2003CA2216399C An elliptical satellite system which emulates the characteristics of geosynchronous satellites
02/03/2003CA2354658A1 Hydrogen combustion robotic propulsion engine
01/2003
01/30/2003US20030023355 Miniature attitude sensing suite
01/30/2003US20030022623 Method for identifying growth limits of handheld services for mobile satellite communications
01/30/2003US20030021628 Screw mounting installation and repair method and apparatus
01/30/2003US20030019977 Propellant utilization system
01/30/2003US20030019180 Foldable member
01/29/2003EP1280228A2 Large membrane space structure and method for its deployment and expansion
01/28/2003US6512979 Lost-in-space stellar attitude acquisition using multiple star trackers
01/28/2003US6511022 Spacecraft solar panel spherical trickle charger
01/28/2003US6511021 Thermal control system for controlling temperature in spacecraft
01/28/2003US6511020 Method for limiting interference between satellite communications systems
01/23/2003WO2003007311A1 Description of methods to increase propellant throughput in a micro pulsed plasma thruster
01/23/2003WO2002041093A3 System and method for implementing a constellation of non-geostationary satellites that does not interfere with the geostationary ring
01/23/2003US20030016186 Inflatable structure, array antenna having inflatable structures,and inflatable structure unfolding method
01/23/2003US20030015625 Extendable/retractable bi-fold solar array
01/23/2003US20030015623 Solid rocket motor bolted thrust takeout structure
01/22/2003EP1207103A4 Method for controlling an aerospace system to put a payload into an orbit
01/22/2003CN1099773C Multiple altitude satillite relay system and method
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