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 TERMINÉ 

RADiation and reliability challenges for electronics used in Space, Avionics, on the Ground and at Accelerators (RADSAGA)

Date du début: 1 mars 2017, Date de fin: 28 févr. 2021,

Reliability and radiation damage issues have a long and important history in the domain of satellites and space missions. Qualification standards were established and expertise was built up in space agencies (ESA), supporting institutes and organizations (CNES, DLR, etc.) as well as universities and specialized companies. During recent years, radiation concerns are gaining attention also in aviati ...
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 9

 TERMINÉ 

Laser Lightning Rod (LLR)

Date du début: 1 janv. 2017, Date de fin: 31 déc. 2020,

Controlling lightning is a long time dream of mankind. The goal of the present project is to investigate and develop a new type of lightning protection based on the use of upward lightning discharges initiated through a high repetition rate multi terawatt laser. The feasibility of the novel technique and the project’s prospect of success are based on recent research providing new insights into the ...
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 9

 TERMINÉ 

Building the next generation high-speed data converters to strengthen European excellence and competitiveness on space applications and beyond (INTERSTELLAR)

Date du début: 1 déc. 2016, Date de fin: 31 août 2020,

...t, the four partners have intimate knowledge in space technology and will bring expertise to the project. E2V (F), coordinator, will be in charge of design, manufacturing and test activities. AIRBUS Defence & Space (UK) and THALES ALENIA SPACE (F), the two major European space companies, will make a key contribution as end-users of space data converters – guiding initial requirements and evaluatin ...
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 4

 TERMINÉ 

Consortium for Hall Effect Orbital Propulsion System (CHEOPS)

Date du début: 1 nov. 2016, Date de fin: 30 avr. 2020,

CHEOPS proposes to develop three different Hall Effect Thruster electric propulsion systems: a dual mode EPS for GEO applications, a low power for LEO applications and a >20 kW high thrust EPS for exploration applications. Each of these will be developed according to market needs and drivers applying incremental technology changes to existing EPS products. The development approach will follow the ...
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 14

 TERMINÉ 

Deep sub-micron microprocessor for spAce rad-Hard appLIcation Asic (DAHLIA)

Date du début: 1 janv. 2017, Date de fin: 31 déc. 2019,

...ng cost and mass and boosting competitiveness of future European space equipments.With the highest cumulative number of European satellites and electronics equipments successfully operating in orbit, Airbus and TAS represent together the indisputable best positioned companies in Europe to ensure the maximum relevance of the DAHLIA SoC for its future use by the whole European Space community. Beyon ...
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 7

 TERMINÉ 

Energy for Smart Objects (EnSO)

Date du début: 1 janv. 2016, Date de fin: 31 déc. 2019,

The goal of EnSO is to develop and consolidate a unique European ecosystem in the field of autonomous micro energy sources (AMES) supporting Electronic European industry to develop innovative products, in particular in IoT markets. In summary, EnSO multi-KET objectives are:• Objective 1: demonstrate the competitiveness of EnSO energy solutions of the targeted Smart Society, Smart Health, and Smart ...
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 36

 TERMINÉ 

demonstRation of EU effective lArge sCale tHreat and crIsis maNaGement OUTside the EU (Reaching out)

Date du début: 1 oct. 2016, Date de fin: 30 nov. 2019,

Effective EU support to a large external crisis requires new approaches. In response to this challenge and to identified user and market needs from previous projects, Reaching Out proposes an innovative multi-disciplinary approach that will optimize the efforts, address a wide spectrum of users and maximize market innovation success.This approach results in five main objectives: to1. Develop a Col ...
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 29

 TERMINÉ 

EnhANcing emergencY management and response to extreme WeatHER and climate Events (ANYWHERE)

Date du début: 1 juin 2016, Date de fin: 31 août 2019,

The ultimate purpose of ANYWHERE is to empower exposed responder institutions and citizens to enhance their anticipation and pro-active capacity of response to face extreme and high-impact weather and climate events. This will be achieved through the operational implementation of cutting-edge innovative technology as the best way to enhance citizen's protection and saving lives.ANYWHERE proposes t ...
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 32

 TERMINÉ 

European Initiative to Enable Validation for Highly Automated Safe and Secure Systems (ENABLE-S3)

Date du début: 1 mai 2016, Date de fin: 30 avr. 2019,

ENABLE-S3 will pave the way for accelerated application of highly automated and autonomous systems in the mobility domains automotive, aerospace, rail and maritime as well as in the health care domain. Virtual testing, verification and coverage-oriented test selection methods will enable validation with reasonable efforts. The resulting validation framework will ensure Europeans Industry competiti ...
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 76

 TERMINÉ 

Efficient Composite parts manufacturing (EFFICOMP)

Date du début: 1 avr. 2016, Date de fin: 31 mars 2019,

...tion of composite parts for structural application on aerospace products. These objectives are fully in line with objectives of the call MG1.8. European partners consortium is composed with end user (AIRBUS Group) and research laboratories (DLR, Stuttgart University, Delft University) and a dissemination expert partner (EASN). All selected partners have a strong experience with aerospace research ...
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 6

 TERMINÉ 

Ecological and Multifunctional Composites for Application in Aircraft Interior and Secondary Structures (ECO-COMPASS)

Date du début: 1 avr. 2016, Date de fin: 31 mars 2019,

Composites are important materials used in aircrafts due to their excellent mechanical properties combined with relatively low weight enabling the reduction of fuel consumption. Expensive carbon fibre reinforced plastics (CFRP) are used in fuselage and wing structures and increasingly replace classic metals. Glass fibre reinforced plastics (GFRP) are mainly used for the interior panels. All these ...
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 9

 TERMINÉ 

Integrated design and novel tooling and process optimisation of microwave processing of composites (SIMUTOOL)

Date du début: 1 sept. 2015, Date de fin: 28 févr. 2019,

SIMUTOOL will develop a simulation platform for the manufacturing of composites through microwave MW heating. The simulation will include the electromagnetic field coupled with heat transfer mechanisms that take place during the production process. It will also include the process control loop which will enable the optimum design of the manufacturing process.One of the major outputs of the simulat ...
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 9

 TERMINÉ 

Validation of European high capacity rad-hard FPGA and software tools (VEGAS)

Date du début: 1 janv. 2016, Date de fin: 31 déc. 2018,

VEGAS proposes to address the key challenge of European non-dependence and competitivness regarding rad-hard FPGA for space applications. VEGAS will evaluate (following ESCC rules) and validate the first rad-hard FPGA in 65nm to directly compete with the US offering and reach TRL 7. The VEGAS project sets clear and measurable main objectives to reach a TRL 7 from TRL 5 (end of BRAVE project) as fo ...
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 11

 TERMINÉ 

Future Sky Safety

Date du début: 1 janv. 2015, Date de fin: 31 déc. 2018,

The EC Flight Path 2050 vision aims to achieve the highest levels of safety to ensure that passengers and freight as well as the air transport system and its infrastructure are protected. However, trends in safety performance over the last decade indicate that the ACARE Vision 2020 safety goal of an 80% reduction of the accident rate is not being achieved. A stronger focus on safety is required. T ...
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 32

 TERMINÉ 

Multi-contact Collaborative Humanoids in Aircraft Manufacturing (COMANOID)

Date du début: 1 janv. 2015, Date de fin: 31 déc. 2018,

COMANOID investigates the deployment of robotic solutions in well-identified Airbus airliner assembly operations that are laborious or tedious for human workers and for which access is impossible for wheeled or rail-ported robotic platforms. As a solution to these constraints a humanoid robot is proposed to achieve the described tasks in real-use cases provided by Airbus Group. At a first glance, ...
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 7

 TERMINÉ 

Towards Demonstration of Photonic Payload For Telecom Satellites (OPTIMA)

Date du début: 1 nov. 2016, Date de fin: 31 oct. 2018,

...bre based equipment.However, great efforts are required to bring these benefits to the world of telecoms payloads as all the photonics equipment used on ground need to be adapted for space.In OPTIMA, Airbus Defence and Space (UK, FR), a world-leading satellite prime manufacturer, will define, assemble and a test photonic payload demonstrator based on building blocks developed, adapted for space an ...
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 9

 TERMINÉ 

PROJET PILOTE FRANCO ALLEMAND POUR UN ERASMUS DES APPRENTIS

Date du début: 1 juin 2016, Date de fin: 31 mai 2018,

Par manque de temps, le résumé n'a pas été traduit.
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 2

 TERMINÉ 

"""2nd Generation Active Wing“ – Active Flow- Loads & Noise control on next generation wing" (AFLONEXT)

Date du début: 1 juin 2013, Date de fin: 31 mai 2018,

AFLoNext is a four year EC L2 project with the objective of proving and maturing highly promising flow control technologies for novel aircraft configurations to achieve a quantum leap in improving aircraft’s performance and thus reducing the environmental footprint. The project consortium is composed by forty European partners from fifteen countries. The work has been broken down into seven work p ...
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 41

 TERMINÉ 

Integrated, Intelligent modular power electronic converter (I2MPECT)

Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,

Increasingly demanding requirements in the transportation industry for higher efficiency and reduced carbon footprint are leading to an ever increasing interest in electrically operated drives which offer significant benefits over their pneumatic or hydraulic counterparts. More electric aircraft technologies with fully electrical actuation and environmental conditioning systems are moving from top ...
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 9

 TERMINÉ 

Aeroelastic Gust Modelling (AEROGUST)

Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,

Encounters with atmospheric turbulence are a vitally important in the design and certification of many manmade structures such as aircraft and wind turbines. Gusts cause rapid changes in the flow about the structures which leads to rigid and flexible unsteady responses. Knowledge of aircraft/gust interactions is therefore vital for loads estimation during aircraft design as it impacts on control s ...
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 13

 TERMINÉ 

Quality assurance concepts for adhesive bonding of aircraft composite structures by advanced NDT (ComBoNDT)

Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,

The integration of innovative lightweight materials like CFRP into multi-material design (MMD) environments in aeronautic applications brings along a paradigm shift in initial design, manufacturing and in maintenance, repair and overhaul (MRO). Essential cost reductions over the whole aircraft lifecycle demand innovative processes meeting the specific requirements of MMD in general and specificall ...
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 14

 TERMINÉ 

SATELLITE-BASED ADS-B FOR LOWER SEPARATION-MINIMA APPLICATION (SALSA) (SALSA)

Date du début: 1 avr. 2016, Date de fin: 31 mars 2018,

SALSA is an exploratory research project relating to multi-source ADS-B system.A multi-source ADS-B system that combines the benefit of all possible type of relays (space, maritime, air or ground based) of ADS-B messages could provide a global surveillance system to overcome the prevailing continuous surveillance constraints in the non-radar airspace (NRA). By bringing Space based ADS-B with othe ...
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 6

 TERMINÉ 

DEMETER

Date du début: 15 sept. 2014, Date de fin: 15 mars 2018,

Title: Deep Submicron System on Chip (SoC) pilot line demonstration for harsh environment applications in Europe300mm wafers manufacturing and 65nm technology for space developed by STm, are a worldwide leading item. The European Space Community needs high complexity radiation-hardened reprogrammable FPGAs allowing dynamic partial reconfiguration (DPR) and providing state of the art, tamper proof, ...
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 14

 TERMINÉ 

Hybrid Propulsion Module for transfer to GEO orbit (HYPROGEO)

Date du début: 1 févr. 2015, Date de fin: 31 janv. 2018,

Independent access to space is a key component of the European Space Policy. The competition is increasing in this area both for the full launching systems and the key subsystems. Cost-effectiveness becomes the main driving factor.HYPROGEO ambition is to study a propulsion module based on Hybrid chemical propulsion. Hybrid propulsion is not a new technology but its application to a transfer module ...
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 15

 TERMINÉ 

THINGS2DO (THINGS2D0)

Date du début: 1 janv. 2014, Date de fin: 1 janv. 2018,

Develop the FDSOI ecosystem in Europe, beyond the PLACES2BE Pilot Line, in order to increase the impact of this European technology. At the time of set up of the first KET pilot line the proof of FDSOI was mainly technological. In between then and now, the first realization of a complex silicon chip in FDSOI has shown to the worldwide microelectronics community the capabilities of this technology. ...
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 44

 TERMINÉ 

European Consortium for Lithium-Sulfur Power for Space Environments (ECLIPSE)

Date du début: 1 déc. 2015, Date de fin: 30 nov. 2017,

...cheaper), non-dependency and innovation: beyond current markets, this breakthrough can enable new challenging missions.The impact of the project is secured by the composition of the consortium led by Airbus Defence and Space with the main European actors of the Lithium-Sulfur electrochemistry and space batteries: ECLIPSE will contribute to the consolidation of an independent European industrial su ...
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 12

 TERMINÉ 

A Low Cost Active Debris Removal Demonstration Mission (REMOVEDEBRIS)

Date du début: 11 nov. 2013, Date de fin: 11 nov. 2017,

A huge amount of debris has progressively been generated since the beginning of the space era. Most of the objects launched into space are still orbiting the Earth and today these object and their by-products represent a threat both in space and on Earth. In Space, debris lead to collisions and therefore to damages to operational satellites. For both issues, a credible solution has emerged over th ...
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 11

 TERMINÉ 

An international network of 50 CubeSats for multi-point, in-situ measurements in the lower thermosphere and re-entry research (QB50)

Date du début: 1 nov. 2011, Date de fin: 31 oct. 2017,

The QB50 Project will demonstrate the possibility of launching a network of 50 CubeSats built by CubeSat teams from all over the world to perform first-class science and in-orbit demonstration in the largely unexplored middle and lower thermosphere. Space agencies are currently not pursuing a multi-spacecraft network for in-situ measurements in the middle and lower thermosphere because the cost of ...
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 17

 TERMINÉ 

Science and Technology for Near-Earth Object Impact Prevention (NEOShield-2)

Date du début: 1 mars 2015, Date de fin: 30 sept. 2017,

Impacts of near-Earth objects (NEOs) have contributed to mass extinctions and evolution, and it is a proven fact that NEOs will continue to hit the Earth at irregular intervals in the future, with the potential for catastrophic damage to life and property. With the experience and results gained from the NEOShield project we are now very well equipped to address all aspects of this call, including ...
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 12

 TERMINÉ 

Avionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraft (ASHLEY)

Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,

In search for a more competitive, multiple types of aircrafts, IMA based, avionics platform solution, the European aerospace industry has recently initiated the IMA2G paradigm thanks to the EC funded SCARLETT project.This latter successfully validated a first underlying set of IMA2G concepts (Separate Core Processing resources from I/O resources, introduce resource segments typology of electronics ...
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 39

 TERMINÉ 

JEt noise of high bypass RatiO eNgine: Installation, advanced Modelling and mitigatiOn (JERONIMO)

Date du début: 1 nov. 2012, Date de fin: 31 août 2017,

The central goal of JERONIMO is the understanding of the physical mechanisms of ultrahigh bypass ratio (UHBR) engines with a bypass ratio (BPR) larger than 12 and the related installed jet noise with potential jet-wing interaction. The aim is to reduce uncertainties in jet noise characterisation of this novel installation configuration by wind tunnel tests and predictions and being able to derive ...
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 13

 TERMINÉ 

Global ATM security management (GAMMA)

Date du début: 1 sept. 2013, Date de fin: 31 août 2017,

The GAMMA project stems from the recognition that while the SESAR initiative is effectively addressing some security issues in the new global ATM scenarios, there is a need to extend this scope to ensure a comprehensive assessment of the full set of security threats and vulnerabilities affecting ATM, considered as a system of systems and covering operational as well as technological aspects. In ad ...
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 23

 TERMINÉ 

SUstainable Network for Japan-Europe aerospace research and Technology cooperation II (SUNJET II)

Date du début: 1 déc. 2014, Date de fin: 31 août 2017,

SUNJET II proposal responds to the H2020-MG-2014 Topic 1.8 International Cooperation in Aeronautics of the work programme. Its main objectives are:• Recommendations and guidance for future EU-Japan cooperation in the field of aviationBuilding on the SUNJET project, SUNJET II will produce consolidated roadmaps in the fields of Aircraft, Systems and Equipment, with the support of R&T institutions, A ...
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 8

 TERMINÉ 

Embedded Multi-Core Systems for Mixed Criticality Applications in Dynamic and Changeable Real-Time Environments (EMC2)

Date du début: 1 avr. 2014, Date de fin: 30 juin 2017,

Embedded systems are the key innovation driver to improve almost all mechatronic products with cheaper and even new functionalities. Furthermore, they strongly support today's information society as inter-system communication enabler.Consequently boundaries of application domains are alleviated and ad-hoc connections and interoperability play an increasing role. At the same time, multi-core and ma ...
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 101

 TERMINÉ 

European Control System Security Incident Analysis Network (ECOSSIAN)

Date du début: 1 juin 2014, Date de fin: 31 mai 2017,

The protection of critical infrastructures increasingly demands solutions which support incident detection and management at the levels of individual CI, across CIs which are depending on each other, and across borders. An approach is required which really integrates functionalities across all these levels. Cooperation of privately operated CIs and public bodies (governments and EU) is difficult b ...
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 22

 TERMINÉ 

Establish Pan-European Information Space to Enhance seCurity of Citziens (EPISECC)

Date du début: 1 juin 2014, Date de fin: 31 mai 2017,

"In a disaster situation three things contribute to a success: having the right resource available in the shortest time, with the highest relevance and at the right location.Access to necessary information, communication with other rescuers and stakeholders as well as the availability of resources are key factors in minimizing damage and loss of life.Large scale disasters and crisis situations inc ...
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 13

 TERMINÉ 

advanced Concept for laser uplink/ downlink CommuniCation with sPace Objects (C3PO)

Date du début: 1 juin 2015, Date de fin: 31 mai 2017,

C3PO: advanced Concept for laser uplink/ downlink CommuniCation with sPace Objects represents a radical improvement in performance of existing ground to low earth orbit communication systems in terms of weight reduction, on-board power consumption, data rate and communication security & confidentiality. C3PO in figures:- Mass reduction by a factor 14- On-board power consumption reduction by a fact ...
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 8

 TERMINÉ 

High Altitude Ice Crystals (HAIC)

Date du début: 1 août 2012, Date de fin: 31 janv. 2017,

Commercial aircraft have been experiencing in-service events while flying in the vicinity of deep convective clouds since at least the early 1990s. Heated probes and engines are the areas of air-craft most prone to mixed phase and glaciated icing threat. In anticipation of regulation changes regarding mixed phase and glaciated icing conditions, the HAIC project will provide the necessary Acceptabl ...
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 40

 TERMINÉ 

Feasibility and Definition of a Triple Core Lockstep ARM System-on-Chip for Space Applications (TCLS ARM FOR SPACE)

Date du début: 1 févr. 2015, Date de fin: 31 déc. 2016,

...udy the portability to European latest and highest performance hardened semiconductor technology (STM65nm)This is achieved by the collaboration of the most experienced companies in this field, namely Airbus Defence and Space (G, F) for specific heritage on high reliable and radiation hardened systems, ARM (UK) providing its excellence in processor core IPs and know-how in this field of development ...
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 6

 TERMINÉ 

Inter System Interoperability for Tetra-TetraPol Networks (ISITEP)

Date du début: 1 sept. 2013, Date de fin: 31 déc. 2016,

A European network where forces share communications, processes and a legal framework would greatly enforce response to disaster recovery and security against crime. Until now, uncertainty on costs, timescale and functionalities has slowed down integration of national Public Protection & Disaster Relief (PPDR) networks. The lack of interoperable communication systems has impeded the cooperation of ...
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 19