| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 09/12/2006 | US7104507 Very safe manned rocket and method of entertaining |
| 09/12/2006 | US7104506 Spacecraft disturbance trimming system |
| 09/12/2006 | US7104505 Autonomous satellite docking system |
| 09/08/2006 | WO2006093715A2 Spacecraft adapter having embedded resources, and methods of forming same |
| 09/08/2006 | WO2006093198A1 Heat transfer thruster |
| 09/08/2006 | WO2006092625A1 Deployable phased array antenna for satellite communications |
| 09/08/2006 | WO2006071207A3 Dynamic cmg array and method |
| 09/06/2006 | EP1697212A2 Dynamic cmg array and method |
| 09/06/2006 | CN2813417Y Lunar vehicle platform |
| 09/06/2006 | CN1827475A Mini-sized large-load SMA space synchronous unlocking mechanism |
| 09/05/2006 | US7102113 Three-axis attitude control propulsion device and flying object comprising the same |
| 09/05/2006 | US7100874 Flexible structural restraint layer for use with an inflatable modular structure |
| 08/31/2006 | US20060192057 Spacecraft adapter having embedded resources, and methods of forming same |
| 08/31/2006 | US20060192056 Virtually geostationary satellite array with optimized parameters |
| 08/31/2006 | DE10234902B4 Thruster-Solar-Segler mit Ring-Segment-Montage-System Thruster solar sailer with ring-segment mounting system |
| 08/30/2006 | EP1696014A2 Electrostatic protection, in particular for use in space |
| 08/30/2006 | CN1824579A Integral vibration isolation platform of astrovehicle |
| 08/30/2006 | CN1824578A Extra long aerated expansion supporting rod for outer space |
| 08/29/2006 | US7097140 System and method for spacecraft attitude control |
| 08/29/2006 | US7097127 Mass trim mechanism |
| 08/24/2006 | US20060186274 Spacecraft power acquisition method for wing-stowed configuration |
| 08/24/2006 | US20060185726 Space-based power system |
| 08/23/2006 | EP1167188B1 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lres) |
| 08/22/2006 | US7096095 Method for the fuel-optimized selection of a thruster configuration |
| 08/22/2006 | US7093806 Method and system for decoupling structural modes to provide consistent control system performance |
| 08/22/2006 | US7093805 System and methods for integrating a payload with a launch vehicle |
| 08/22/2006 | US7093804 Foldable and deployable assembly of elements mounted on board a spacecraft |
| 08/22/2006 | US7093800 Method of operating a satellite for end-of-life maneuvers |
| 08/22/2006 | US7093787 Lightning strike mitigation system |
| 08/22/2006 | US7093617 Fluidic diverter valve with a non-spherical shuttle element |
| 08/17/2006 | US20060180707 Spacecrafts sculpted by solar beam and protected with diamond skin in space |
| 08/17/2006 | US20060180706 Method for seizing an object |
| 08/17/2006 | DE10318885B4 Vorrichtung zum Stauen und Entfalten von Foliensystemen Apparatus for stowing and deploying film systems |
| 08/17/2006 | DE102005005934A1 Ramjet engine operating method, involves utilizing hydrosilicon mixture in hot combustion chamber, where mixture disintegrates into atomic hydrogen and silicon and twenty one percent of oxygen portion in air is burned stoichiometrically |
| 08/16/2006 | CN1818402A Product with multiple functions |
| 08/15/2006 | US7090171 Momentum stabilized launch vehicle upper stage |
| 08/15/2006 | US7090170 In-orbit satellite sensor alignment determination |
| 08/10/2006 | US20060179456 Satellite information autonomous distribution satellite, satellite information collecting system, and satellite terrestrial test system |
| 08/10/2006 | DE102005005156A1 Engine for e.g. satellite drive system, has combustion chamber that is downstream to decomposition chamber, where outlet of combustion chamber is connected with inlet of expansion nozzle |
| 08/10/2006 | DE102005004922A1 Solarzellenausleger Solar boom |
| 08/09/2006 | EP1688350A2 Solar array |
| 08/03/2006 | WO2002086317A8 Antimatter engine |
| 08/03/2006 | US20060169846 Micro-optics concentrator for solar power satellites |
| 08/03/2006 | US20060169845 In-orbit satellite sensor alignment determination |
| 08/03/2006 | US20060169844 Coating for prevention of electrostatic discharge within an equipment in a spatial environment |
| 08/02/2006 | EP1631747A4 Fastener for air bags and other uses |
| 08/01/2006 | US7084572 Plasma-accelerator configuration |
| 07/27/2006 | US20060165479 Coupling device |
| 07/27/2006 | US20060163434 Spacecraft for interplanetary/lunar travel |
| 07/25/2006 | US7080809 Space transportation system |
| 07/20/2006 | WO2006075343A1 Instability control system for magneto-plasma-dynamic thrusters (mpdt) |
| 07/20/2006 | DE202006003251U1 Low-power powder electro rocket motor for e.g. re-orientation or stabilization of artificial earth satellite or deep space exploration probe |
| 07/19/2006 | EP1680648A1 Method of controlling the attitude of satellites, particularly agile satellites with a reduced number of gyrodynes |
| 07/19/2006 | EP1680645A1 Composite structural part comprising pyrotechnic detonating rupture means |
| 07/19/2006 | EP1680607A2 Non-pyrolytically actuated reduced-shock separation fastener |
| 07/18/2006 | US7078880 Energy storage flywheel voltage regulation and load sharing system and method |
| 07/18/2006 | US7077361 Micro-optics concentrator for solar power satellites |
| 07/13/2006 | WO2006073381A1 Method and apparatus for quantum vortex implosion propulsion and species |
| 07/13/2006 | US20060151671 Actuator arm for use in a spacecraft |
| 07/13/2006 | DE10316131B4 Versorgungs- und Inspektionsvorrichtung für Kleinplattformen im Orbit Supply and inspection equipment for small platforms in orbit |
| 07/13/2006 | DE102005021459B3 Mechanical rotation drive with rod-like torsion element |
| 07/12/2006 | EP1679259A2 Method of injecting plurality of spacecrafts into different orbits individually |
| 07/12/2006 | EP1678034A1 Payload launching system |
| 07/11/2006 | US7076341 Autonomous manoeuvring for spinning spacecraft |
| 07/11/2006 | US7075048 Omni-directional radiation source and object locator |
| 07/11/2006 | CA2458548C Solar array concentrator system and method |
| 07/06/2006 | WO2006071207A2 Dynamic cmg array and method |
| 07/06/2006 | WO2006070156A1 Support device for elements on a piece of space equipment with flexible deploying arms |
| 07/06/2006 | US20060145052 Method and apparatus for assigning weighting coefficinents for performing attitude calculations with a star sensor |
| 07/06/2006 | US20060145026 Attenuation device |
| 07/06/2006 | US20060145025 Method for aerial rearmament of aircraft |
| 07/06/2006 | US20060145024 Service vehicle for performing in-space operations on a target spacecraft, servicing system and method for using a service vehicle |
| 07/06/2006 | US20060145023 Geometrically encoded magnetic latch intercontact face |
| 07/06/2006 | US20060145022 Propellant tank baffle system |
| 07/06/2006 | US20060145021 Composite shell spacecraft seat |
| 07/06/2006 | US20060145020 Atmospheric entry thermal protection system |
| 07/06/2006 | US20060145019 Triangular spacecraft |
| 07/06/2006 | US20060145018 Unitized hybrid rocket system |
| 07/06/2006 | US20060145017 Optimized land mobile satellite system for north american coverage |
| 07/06/2006 | US20060145016 Mating of spacecraft components using shape memory materials |
| 07/06/2006 | DE10357902B4 Verfahren zum Befüllen eines Behälters und Verfahren zum Herstellen einer monophasigen Lösung in Schwerelosigkeit A method for filling a container and method for producing a monophase solution in weightlessness |
| 07/06/2006 | DE10160020B4 Vorrichtung zum Bestimmen der Zielrichtung, in der ein von einer Quelle erzeugter Strahl gesendet wird und mit einer solchen Vorrichtung ausgestatteter Satellit Apparatus for determining the target direction in which a generated beam is transmitted from a source and equipped with such a device satellite |
| 07/05/2006 | EP1676777A1 Satellite equipped with means for countering the solar pressure |
| 07/05/2006 | EP1676776A1 Device for supporting elements of a spacecraft equipment with flexible deployable blades |
| 07/05/2006 | EP1676093A2 Low shock separation joint and method therefore |
| 07/05/2006 | EP1675770A1 Low shock separation joint and method of operation |
| 07/05/2006 | CN2792948Y Thermal insulator of spacecraft |
| 07/05/2006 | CN1798929A Fastener for air bags and other uses |
| 07/05/2006 | CN1796229A Flying disk of annular engine |
| 07/04/2006 | US7070151 In orbit space transportation and recovery system |
| 07/04/2006 | US7069975 Method and apparatus for cooling with a phase change material and heat pipes |
| 06/29/2006 | WO2006068884A1 Geometrically encoded magnetic latch intercontact face |
| 06/29/2006 | WO2006067354A1 Flexible electrochemical cell with controlled optical absorption and reflection having an aqueous electrolyte |
| 06/29/2006 | WO2006067352A1 Electrochemical cell with optical absorption and reflection controlled by copper electroplating |
| 06/29/2006 | WO2006067078A2 Coating for prevention of electrostatic discharge within an equipment in a spatial environment |
| 06/29/2006 | WO2006066296A1 Retainer bracket for the arm of an extending jib of a space vehicle |
| 06/29/2006 | US20060141954 Slice based architecture for a multifunction radio |
| 06/29/2006 | US20060138966 Ion accelerator arrangement |
| 06/29/2006 | US20060138284 Apparatus with axis-parallel tension cables for ejecting a spin-stabilized body from a spacecraft |
| 06/29/2006 | US20060138283 Apparatus with helical tension cables for ejecting a spin-stabilized body from a spacecraft |