| Patents for B64G 1 - Cosmonautic vehicles (11,089) |
|---|
| 05/03/2005 | US6888073 Vibration absorbing system of micro gravity rotating apparatus |
| 05/03/2005 | US6886790 Stand-off for fixing thermal protection panels |
| 04/28/2005 | WO2005037646A2 Precision attitude control system for gimbaled thruster |
| 04/28/2005 | US20050090948 Process for determining the position of a spacecraft with the aid of a directional vector and a total angular momentum measurement |
| 04/28/2005 | US20050090569 Structure including a plurality of cells of cured resinous material, method of forming the structure and apparatus for forming the structure |
| 04/28/2005 | US20050089661 Cryogenic fuel tank insulation assembly |
| 04/27/2005 | EP1526073A1 Equipment to nullify gravitational force |
| 04/27/2005 | EP1526072A1 Dynamic yaw steering method for spacecraft |
| 04/27/2005 | CN1610628A Space craft with extensible radiators |
| 04/26/2005 | US6883757 System and method for increasing the roll offset operating range for a spacecraft |
| 04/26/2005 | US6883588 Spacecraft radiator system using a heat pump |
| 04/26/2005 | US6883543 Pulse detonation engine having an aerodynamic valve |
| 04/21/2005 | WO2005035363A1 A thruster for propelling and directing a vehicle without interacting with environment and method for making the same |
| 04/21/2005 | WO2005035362A1 Cargo transport means |
| 04/21/2005 | US20050084665 Thermal insulation system employing oxide ceramic matrix composites |
| 04/21/2005 | US20050084364 Non-pyrolytically actuated reduced-shock separation fastener |
| 04/21/2005 | US20050082424 Flying vehicle-launching apparatus and method |
| 04/21/2005 | US20050082038 Apparatus for cooling components in spacecraft |
| 04/20/2005 | EP1252061B1 Twin lobe spacecraft dispenser apparatus and method |
| 04/20/2005 | CN1607749A Communication system |
| 04/14/2005 | WO2005033498A1 Aerospace laser jet engine |
| 04/14/2005 | US20050080521 Method for the fuel-optimized selection of a thruster configuration |
| 04/14/2005 | US20050077433 Apparatus and method for maneuvering objects in low/zero gravity environments |
| 04/14/2005 | US20050077432 Dual conduction heat dissipating system for a spacecraft |
| 04/14/2005 | US20050077425 Thruster for propelling and directing a vehicle without interacting with environment and method for making the same |
| 04/14/2005 | DE202004002176U1 Parachute for descent or braking used in aerospace vehicle, includes inflatable chambers with double-walled construction |
| 04/13/2005 | CN1606517A Plasma-accelerator configuration |
| 04/07/2005 | WO2005017561A3 Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits |
| 04/06/2005 | EP1519833A1 Product and method for producing a non-woven fabric by means of hydrodynamic needling |
| 04/06/2005 | CN1603599A Minisize chemical propeller with pressure sensor |
| 04/05/2005 | US6876714 Device for heating gas from a thin layer of nuclear fuel, and space engine incorporating such device |
| 04/05/2005 | US6874434 Biomass waste disposal method and apparatus |
| 04/05/2005 | CA2142265C Vibration reduction |
| 03/31/2005 | WO2005029927A2 Pulsed plasma accelerator and method |
| 03/31/2005 | WO2005028309A2 Solar wind-driven craft |
| 03/31/2005 | US20050071055 Refinement of spacecraft angular velocity and attitude estimates using star data |
| 03/31/2005 | US20050071054 Onboard satellite processing to mitigate data recorder limits |
| 03/31/2005 | US20050067534 Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking |
| 03/31/2005 | US20050067524 Method and system for accelerating an object |
| 03/31/2005 | DE19945586B4 Verwendung eines Thermalschutzsystems Use of a thermal protection system |
| 03/30/2005 | EP1518057A2 Method and system for decoupling structural modes to provide consistent control system performance |
| 03/29/2005 | US6873886 Modular mission payload control software |
| 03/24/2005 | WO2005000574A3 Positive pressure hot bonder |
| 03/24/2005 | WO2004106268A3 Explosive devices |
| 03/24/2005 | US20050064165 Acoustically damped composite construction for the forward portion of a rocket or missile |
| 03/24/2005 | US20050063252 Method for the detection of damage to spacecraft caused by the impact of foreign bodies |
| 03/24/2005 | US20050061957 Laser range finder |
| 03/24/2005 | US20050061920 Energy storage flywheel retention system and method |
| 03/24/2005 | US20050061919 Method for use of external secondary payloads |
| 03/24/2005 | US20050061918 Method for making an opening in the bladder of an inflatable modular structure for receiving a window |
| 03/24/2005 | US20050061908 Shock wave modification method and system |
| 03/24/2005 | DE19642407B4 Vorrichtung für die Lageregelung eines Raumflugkörpers mittels Betätigung eines Gasventils mit beweglicher Düse Device for attitude control of a spacecraft by operation of a gas valve with a movable nozzle |
| 03/24/2005 | DE10208240B4 Satellit mit einer Radiatorfläche Satellite with a radiator surface |
| 03/23/2005 | EP1516815A1 Device for grasping objects in outer space |
| 03/23/2005 | EP1516814A1 Recovery device |
| 03/23/2005 | EP1165371B1 System for controlling the attitude of a spacecraft |
| 03/22/2005 | US6869048 De-orbit instrument package |
| 03/18/2005 | CA2441505A1 Lift-providing unit for levitating a platform |
| 03/17/2005 | US20050060474 Centralized bus interface with single wire secondary distribution |
| 03/17/2005 | US20050060092 Laser range finder closed-loop pointing technology of relative navigation, attitude determination, pointing and tracking for spacecraft rendezvous |
| 03/17/2005 | US20050056729 Particle accelerator space engine |
| 03/17/2005 | US20050056509 Shock isolation system |
| 03/17/2005 | DE10350734B3 Solar-thermal drive unit for rocket propulsion system has hollow chamber body and heating channel system |
| 03/17/2005 | DE10337973A1 Auswurfvorrichtung für drallstabilisierte Raumflugkörper Ejection device for spin-stabilized spacecraft |
| 03/16/2005 | EP1514799A1 Method for attitude determination of spacecraft using a direction vector and a total momentum measurement |
| 03/16/2005 | CN1594034A Lift force providing unit and delivery vehicle having the same |
| 03/15/2005 | US6868316 Satellite constellation system |
| 03/15/2005 | US6867391 Control system for electrostatic discharge mitigation |
| 03/15/2005 | US6866232 Automated docking of space vehicle |
| 03/15/2005 | US6866231 Method for limiting interference between satellite communications systems |
| 03/10/2005 | WO2005021379A1 Inertia wheel for space vehicle |
| 03/10/2005 | WO2004092013A3 Winged spacecraft |
| 03/10/2005 | US20050051670 Device and method for on-orbit calibration verification of an infrared sensor |
| 03/10/2005 | US20050050841 Stacking tie-rod release device for a deployable structure |
| 03/09/2005 | EP1512233A2 A highly elliptical orbit for communications satellites |
| 03/09/2005 | CN1590219A Flying disk |
| 03/09/2005 | CN1191947C Electric vehicle with variable efficiency regenerative braking depending upon battery charge state |
| 03/08/2005 | US6863408 Hinge assembly for deploying the petals of a sectored mirror of an optical space telescope |
| 03/08/2005 | US6863244 Mitigation of angular acceleration effects on optical sensor data |
| 03/08/2005 | US6863190 Protective enclosure for use transporting orbital replacement units (orus) within a space craft |
| 03/03/2005 | WO2004032392A3 Steering logic for control moment gyro system |
| 03/03/2005 | US20050049764 Momentum estimator for on-station momentum control |
| 03/03/2005 | US20050045773 System for ejecting a spin-stabilized space flying body |
| 03/03/2005 | US20050045772 Reusable launch system |
| 03/03/2005 | US20050045771 Compact external launcher for small space payloads |
| 03/03/2005 | US20050045306 Transpiration cooling system |
| 03/03/2005 | DE10033093B4 Vorrichtung zum lösbaren verbinden rotationssystemmetrischer Bauteile Means for releasably connecting rotationssystemmetrischer components |
| 03/02/2005 | EP1510458A1 Lift thruster for levitating a platform |
| 03/02/2005 | CN1191429C Elastomerized phenolic resin ablative insulation for rocket motors |
| 03/01/2005 | US6860451 Spacecraft spin axis reorientation method |
| 03/01/2005 | US6860166 Torque induced propulsion system |
| 02/24/2005 | WO2005017561A2 Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits |
| 02/24/2005 | WO2005016756A1 Reaction wheel system with vernier control rotor |
| 02/24/2005 | WO2005016746A1 Disc flying object |
| 02/24/2005 | US20050040921 Apparatus for control of uniform gravity utilizing superconducting magnet |
| 02/24/2005 | US20050040282 Apparatus for a geosynchronous life extension spacecraft |
| 02/24/2005 | US20050039557 Linear actuation device for spacecraft and solar generator unfolding systems |
| 02/24/2005 | DE10334352A1 Solargenerator zur Entfaltung in zwei Raumrichtungen Solar generator for deployment in two spatial directions |
| 02/23/2005 | EP1508518A1 Ejector for spin-stabilised space vehicles |
| 02/23/2005 | EP1507705A2 Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking |