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Astrium Sas
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Astrium Sas patents

Recent patent applications related to Astrium Sas. Astrium Sas is listed as an Agent/Assignee. Note: Astrium Sas may have other listings under different names/spellings. We're not affiliated with Astrium Sas, we're just tracking patents.

ARCHIVE: New 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Astrium Sas-related inventors




Date Astrium Sas patents (updated weekly) - BOOKMARK this page
06/23/16Combustion gas discharge nozzle for a rocket engine provided with a sealing device between a stationary part and a moving part of the nozzle
12/17/15Device for retaining a tank in an aircraft
03/26/15Stabilization of a line of sight of an on-board satellite imaging system
01/01/15Method of controlling the attitude of a satellite and an attitude-controlled satellite
01/01/15Cooling device for regulating the temperature of a heat source of a satellite, and producing the associated cooling device and satellite
01/01/15Method for draping composite materials on a form and material suitable for said method
12/18/14Fourier-transform interferometer with self-apodization compensation
12/18/14Method and system for estimating a path-length difference of a target signal transmitted by a spacecraft or aircraft
10/30/14Flame resistant shield
10/02/14Method for managing service policy in a telecommunications network
08/21/14System and detecting and locating an insulation flaw in a solar generator on a space vehicle
05/29/14Toolset and producing a metal liner
05/29/14Method and device for detecting congestion on a transmission link
05/08/14Detonating pyrotechnic rupture piece
05/08/14Device and optimizing the ground coverage of a hybrid space system
04/24/14Method for making a sandwich type composite by co-firing
04/24/14Aerodynamic and spatial composite flight aircraft, and related piloting method
04/24/14Unknown
04/17/14Satellite communication system, leo satellite relaying communications between a geo satellite and terrestrial stations, the uplinks and downlinks using the same frequency band and time-division multiplexing
02/13/14Method for temporarily connecting two parts together, such as two stages of a space launcher, and assembly including two temporarily connected parts
01/30/14Method and device for the successive launching of two satellites
01/16/14System and managing communications of at least one terminal in a communication network
12/26/13Reversible detonating pyrotechnic rupture piece
12/19/13Method and system for free-field optical transmission by means of laser signals
11/21/13Method and system for piloting a flying craft with rear propulsion unit
11/14/13Network of switches and payload of telecommunications satellite comprising a network of switches
11/07/13Device for monitoring the attitude of a satellite, and controlling a satellite provided with said device
10/24/13Space survey system for monitoring near-earth space
10/10/13Optical surveillance system for a space survey system for monitoring near-earth space
10/03/13Method of using an image sensor
09/19/13System for orienting and positioning an electromagnetic receiver
09/12/13Method and device for non-destructive testing of wind turbine blades
08/29/13Service admission path control (sapc)
08/15/13Heat-protection material
08/15/13Heat-protection material
08/15/13Method for realizing a space survey system for monitoring near-earth space
08/08/13Attachment device with pyrotechnic bolt
08/01/13Optimized heat-protection material
07/25/13Heat transfer system
07/25/13Connection between a metal liner and a composite structure in the mounting region of a tank
05/02/13Method of commanding an attitude control system and attitude control system of a space vehicle
04/25/13Satellite having a simplified, streamlined, and economical structure, and implementing same
04/11/13Simplified reusable module for launcher
04/11/13Permanent-magnet electric motor comprising a segmented stator
02/28/13Polychromatic imaging method
02/28/13Imaging method
12/27/12Ultra-rapid air vehicle and related aerial locomotion
12/13/12Reconfigurable inverter having failure tolerance for powering a synchronous poly-phase motor having permanent magnets, and assembly including said inverter and motor
12/06/12Method for estimating the movement of a traveling observation instrument flying over a celestial body
11/29/12Hybrid space system based on a constellation of low-orbit satellites working as space repeaters for improving the transmission and reception of geostationary signals
11/29/12Replacement part for satellite optical solar reflectors
11/22/12Method for producing a composite mirror and composite mirror obtained with same
11/15/12Method for calibrating thresholds and threshold calibration module for a satellite telecommunications system
11/08/12Method of determining the particle sensitivity of electronic components
08/23/12System comprising a spatial mother probe forming a spatial carrier vehicle and a plurality of spatial daughter probes
07/19/12Virtual polar satellite ground station for low orbit earth observation satellites based on a geostationary satellite pointing an antenna over an earth pole
06/21/12Landing system for a body and space probe provided with such a system
06/14/12Method for detecting shifts in line images obtained by a sensor that is airborne or moving in space
06/07/12Device for assembling sections of wind-turbine blades and linking sections of wind-turbine blades
05/31/12Method for making mechanical links
05/10/12Smooth linear separation device between a first part and a second part
05/10/12Device for temporarily connecting and pyrotechnically separating two assemblies
04/05/12Landing device for a space probe, and landing a probe provided with such a device
03/22/12Method for estimating the motion of a carrier relative to an environment and computing device for navigation system
02/23/12Absorbent dome for a radiating collector tube
Patent Packs
02/09/12Device for measuring the temperature of a substrate
02/02/12Radio antenna
02/02/12Radio antenna with improved decoupling angles
01/26/12Radio antenna including improved means of rigidification
12/29/11Apparatus for producing and dispensing hydrogen
12/08/11Reusable module for launcher
09/22/11Method for protecting composite structures against impacts
09/01/11Thermal control device with network of interconnected capillary heat pipes
08/11/11Passive device with micro capillary pumped fluid loop
06/30/11Method for controlling satellite attitude, and attitude-controlled satellite
06/09/11Device for generating impacts with a structure
06/02/11Spacers for rolling bearings with adjusted lengths
03/31/11Multi-beam satellite telecommunications forming beams
03/24/11Electric thruster for a spacecraft
03/03/11Device for measuring the line of sight jitter of an optical instrument
Patent Packs
02/03/11Device for reducing aerodynamic drag
01/13/11Actuator device for varying the attitude of a spacecraft
12/30/10Spacecraft afterbody device
12/16/10Device for testing structural panels
12/16/10Actuator with transfer of angular momentum for the attitude control of a spacecraft
12/09/10Space vehicle seat and space vehicle provided with this seat
10/21/10Thermal regulation passive device with micro capillary pumped fluid loop
10/21/10Modular device for multi-axial insulation against vibration and impacts, based on elastomer
07/22/10System for positioning a terrestrial user
07/01/10Assembly of prepregs for producing structures, for example ones which deploy through inflation
06/24/10Optical transceiver assembly with transmission-direction control
04/15/10Process for improving the adhesion of carbon fibres with regard to an organic matrix
04/01/10Deployable light structure capable of being rigidified after deployment, its production process and its application to equipping a spacecraft
01/14/10Control moment gyro and device for assembly thereof
01/07/10Device for controlling the heat flows in a spacecraft and spacecraft equipped with such a device
11/26/09Capillary pumped diphasic fluid loop passive thermal control device with thermal capacitor
09/17/09Method of launching into operational orbit an artificial satellite and associated propulsion device
09/03/09Satellite air brake wing structure
08/13/09Control device for deployment of inflatable structures
08/06/09Methods and system for determining angles of sight between two devices
06/25/09Electrical power supply system for a satellite
06/11/09Methods for controlling a rechargeable battery and rechargeable battery for carrying out said method
05/21/09Actuator control reducing the level of vibration of an associated flexible structure
03/19/09Rigidification of structures to be deployed by inflating, particularly for use in space
01/14/10Control moment gyro and device for assembly thereof
01/07/10Device for controlling the heat flows in a spacecraft and spacecraft equipped with such a device







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