Patents for B64G 1 - Cosmonautic vehicles (11,089)
10/2000
10/31/2000US6138951 Spacecraft dispensing system
10/29/2000CA2307384A1 Emergency exit system
10/26/2000WO2000063646A1 Autonomous satellite navigation system
10/24/2000US6138061 Onboard orbit propagation using quaternions
10/24/2000US6137171 Lightweight miniaturized integrated microsatellite employing advanced semiconductor processing and packaging technology
10/24/2000US6136418 Rapidly removable thermal protection system for reusable launch vehicle
10/24/2000US6135394 Practical method and apparatus for satellite stationkeeping
10/24/2000US6135393 Spacecraft attitude and velocity control thruster system
10/24/2000US6135392 Spacecraft attitude control actuator and method
10/24/2000US6135391 Retention system for a detachable spacecraft capsule mounted on a spacecraft
10/24/2000US6135390 Whole-spacecraft hybrid isolation system for launch vehicles
10/24/2000US6135389 Subterranean target steering strategy
10/24/2000US6134782 Method of forming a rocket thrust chamber
10/19/2000WO2000062017A2 An angular rate and reaction torque assembly
10/19/2000WO2000061894A2 Space erected inflatable structure
10/18/2000EP1044352A1 Rotational speed measurement device for rotating missiles
10/18/2000EP0815658A4 An elliptical satellite system which emulates the characteristics of geosynchronous satellites
10/18/2000CN1270304A Disposable launching vehicle
10/17/2000US6133997 System for spotting moving objects based on a plurality of artificial satellites
10/17/2000US6131858 Compact single-propellant unitary propulsion system for a small satellite
10/17/2000US6131857 Miniature spacecraft
10/17/2000US6131646 Heat conductive interface material
10/17/2000US6131397 Slush producing process and device
10/17/2000US6131395 Propellant densification apparatus and method
10/17/2000US6131385 Integrated pulsed propulsion system for microsatellite
10/12/2000WO2000059783A2 Reusable, separable, structural connector assembly
10/12/2000DE19913048A1 Niederhalter für Satelliten-Solargeneratoren Card holders for satellite solar generators
10/11/2000EP1043228A2 D-wing deployable solar array
10/11/2000EP1043227A2 An expendable launch vehicle
10/11/2000EP1042167A1 Satellite angular momentum control system using flywheels supported by superconductor magnetic bearings
10/10/2000US6131058 Process for identifying an incorrectly measuring sensor in a spacecraft
10/10/2000US6131056 Continuous attitude control that avoids CMG array singularities
10/10/2000US6129315 Independent launch lock mechanism
10/05/2000WO2000058989A1 Plasma gun and methods for the use thereof
10/05/2000WO2000057685A2 Method of linear actuation by inflation and apparatus therefor
10/05/2000WO2000013971A9 Fast resonance shifting as a way to reduce propellant for space mission applications
10/04/2000EP1041665A1 Microwave strip transmission lines for satellite antennas
10/04/2000EP1041003A2 Heat insulating material
10/04/2000EP1041002A2 Protective casing with cooling for equipment in air, space or land vehicles
10/04/2000EP1040736A1 Synthetic jet actuators for cooling heated bodies and environments
10/04/2000EP1040312A1 Separation system
10/04/2000EP1040274A1 Pump with positive displacement
10/03/2000US6128575 Methods for accurately inserting satellite constellations into common orbit planes
10/03/2000US6128556 CMG control based on angular momentum to control satellite attitude
10/03/2000US6128555 In situ method and system for autonomous fault detection, isolation and recovery
10/03/2000US6128426 High speed bi-directional optical rotary joint
10/03/2000US6126371 Shape memory metal alloy preload attenuation device
10/03/2000US6126117 State control device of moving body and its state control method
10/03/2000US6126116 Coordinatable system of inclined eccentric geosynchronous orbits
10/03/2000US6126115 Apparatus for retaining and releasing a payload
09/2000
09/28/2000WO2000056604A1 Device for holding down moving elements of a satellite, especially satellite solar generators
09/28/2000WO2000043267A3 Payload carry and launch system
09/28/2000DE19911857A1 Ausstoßmechanismus für Satelliten Ejection mechanism for satellite
09/27/2000EP1038772A2 Satellite dispenser
09/27/2000CN1267616A Method of reducing power consumption of rocket for launching satellite during initial flying stage
09/26/2000US6125310 Thruster on time signaling with flexure compensation avoidance
09/26/2000US6124835 Deployment of dual reflector systems
09/26/2000US6124378 Spacecraft with article overlying the skin comprising particles of a mixed oxide of magnesium or cadmium, aluminum and gallium mixed with an organic binder; low solar absorptance, may be electroconductive by doping
09/26/2000US6123295 Fuel tank for lifting body re-entry vehicle
09/26/2000US6123145 Synthetic jet actuators for cooling heated bodies and environments
09/26/2000US6123026 System and method for increasing the durability of a sapphire window in high stress environments
09/20/2000EP1037404A2 Elliptical satellite communication system
09/20/2000EP1036735A2 Satellite expulsion mechanism
09/20/2000EP0941204A4 Spacecraft yaw pointing for inclined orbits
09/20/2000CN1266800A Communication system, communication receiving device and communication terminal in said system
09/19/2000US6122596 Non-geostationary orbit satelite constellation for continuous preferential coverage of northern latitudes
09/19/2000US6119986 Thin-film solar reflectors and methods
09/19/2000US6119985 Reusable rocket-propelled high altitude airplane and method and apparatus for mid-air oxidizer transfer to said airplane
09/19/2000US6119984 Low shock anti-friction release device
09/19/2000US6119983 Airship/spacecraft
09/19/2000US6119573 Carbon fiber flocking for thermal management of compact missile electronics
09/18/2000CA2266281A1 Optical intersatellite communications system
09/18/2000CA2266155A1 Multimedia satellite constellation network
09/18/2000CA2266154A1 Satellite based earth fixed cell tracking method
09/18/2000CA2266153A1 Multi-media satellite
09/18/2000CA2266132A1 Satellite communication system
09/14/2000WO2000054088A1 Telescope and movement control device
09/14/2000WO2000053377A1 Working robot
09/13/2000EP1035017A1 Method for the simulation of the external thermal flows absorbed by spacecraft external radiator elements in flight and spacecraft for the application of said method
09/13/2000EP0815634B1 Magnetically mounted, position-stabilised flywheel
09/12/2000US6118067 Method and apparatus for improved solar concentration arrays
09/12/2000US6116545 Free return lunar flyby transfer method for geosynchronous satellites
09/12/2000US6116544 Electrodynamic tether and method of use
09/12/2000US6116543 Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse
09/12/2000US6116368 Electric vehicle with battery regeneration dependent on battery charge state
09/08/2000WO2000051887A1 Functionally and structurally modular parallelogram-shaped spacecraft
09/07/2000DE19909167A1 Wärmefluß-Koppelungs-Mechanismus zur Verwendung in der Raumfahrt Heat flux Coupling mechanism for use in space
09/07/2000DE19908683A1 Radiatorstruktur eines Satelliten Radiator structure of a satellite
09/06/2000EP1033829A2 Supplemental satellite communication enhancement technique
09/06/2000EP1033828A2 Supplemental satellite function enhancement technique
09/06/2000EP1033543A2 Slush producing process and device
09/06/2000EP1033542A2 Cryogenic liquid heat exchanger system with fluid ejector
09/06/2000EP1033303A2 Cryogenic densification through introduction of a second cryogenic fluid
09/06/2000EP1033302A2 Heat transfer coupling mechanism for space applications
09/06/2000EP1033301A2 Combined diffuser and recirculation manifold in a propellant or oxidizer tank
09/06/2000EP1033300A2 Method and apparatus for controlling spacecraft attitude with rotational star trackers
09/05/2000US6113035 Attitude control by modulating the rate of propellant depletion
09/05/2000US6113034 Method and apparatus for estimating effects of disturbance forces
09/05/2000US6113033 Combined flywheel energy storage and attitude control apparatus for spacecraft
09/05/2000US6113032 Delivering liquid propellant in a reusable booster stage
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