ASTRIUM SAS
89Patents
81Active
89Granted
56Portfolio score
Filing activity: Oct 19, 1999 → Nov 21, 2013 · 49 expiring within 5 years
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| USD589867S1 | Airplane | General | 19 | Expired |
| USD589868S1 | Airplane | General | 16 | Expired |
| US8360368B2 | Space vehicle seat and space vehicle provided with this seat | Performing Operations; Transporting | 13 | Active |
| US6381007B2 | Photosensitive charge-accumulating device and a lidar incorporating such a device | Electricity | 10 | Expired |
| US8430361B2 | Method and device enabling a rocket engine pump to be driven by an internal combustion engine | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8240612B2 | Device for controlling the heat flows in a spacecraft and spacecraft equipped with such a device | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US6988278B2 | Process and system for video on demand | Electricity | 9 | Expired |
| US6439510B1 | Electrical energy management and attitude control system for a satellite | Performing Operations; Transporting | 8 | Expired |
| US6166515A | Electrical power supply circuit having a solar generator and a battery | Electricity | 8 | Expired |
| US8939396B2 | High-altitude, aerial network for the production and distribution of liquid-hydrogen | Emerging Cross-Sectional Technologies | 8 | Active |
| US9027481B2 | Detonating pyrotechnic rupture piece | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US8136765B2 | Method of launching into operational orbit an artificial satellite and associated propulsion device | Performing Operations; Transporting | 7 | Active |
| US8607706B2 | Device for temporarily connecting and pyrotechnically separating two assemblies | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8399064B2 | Process for improving the adhesion of carbon fibres with regard to an organic matrix | Textiles; Paper | 6 | Active |
| US8844876B2 | Simplified reusable module for launcher | Performing Operations; Transporting | 6 | Active |
| US9174749B2 | Reusable module for launcher | Performing Operations; Transporting | 6 | Active |
| US8505853B2 | Method for controlling satellite attitude, and attitude-controlled satellite | Performing Operations; Transporting | 5 | Active |
| US9562870B2 | Method and device for non-destructive testing of wind turbine blades | Emerging Cross-Sectional Technologies | 5 | Active |
| US8408042B2 | Device for generating impacts with a structure | Physics | 5 | Active |
| US8717234B2 | System for monitoring a satellite constellation of a positioning system | Physics | 5 | Active |
| US8365610B2 | Testing device for structural panels | Physics | 5 | Active |
| US9079661B2 | Ultra-rapid air vehicle and related method for aerial locomotion | Emerging Cross-Sectional Technologies | 5 | Active |
| US9086260B2 | Pyrotechnique rupture method and components for implementing it | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9073646B2 | System comprising a spatial mother probe forming a spatial carrier vehicle and a plurality of spatial daughter probes | Performing Operations; Transporting | 4 | Active |
| US8328977B2 | Method for enhancing adherence of carbon fibers with respect to an organic matrix | Textiles; Paper | 4 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.