Projects

This page displays all ARTES projects except ARTES 20 IAP, which can be found on ARTES Applications - Projects.


Displaying 51 - 100 of 1063

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  • LPGAN

    Status date: 20 April 2017

    Magnitude Space is building a nano‐satellite platform to provide low‐cost IoT data connectivity for sensors globally. In an open development environment, sensors will be integrated with small transmission hardware to send small packets of data to a low‐cost cube-sat constellation and from there via ground stations to data servers at the customers’ premise.

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  • GPV (Gas Passivation Valve)

    Status date: 12 April 2017

    In the frame of space debris mitigation, ESA has implemented new requirements and recommendations, which state that satellite propulsion systems shall be passivated at end of life. The main objective of the project is to develop a Gas Passivation Valve (GPV) to meet applicable passivation requirements related to the existing European Geostationary Telecoms platforms.

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  • SPECSI

    Status date: 11 April 2017

    The SPECSI project examined the role of satellites in future communication networks and applications in 2020-25. It studied emerging ICT trends to identify future opportunities for satcom and their associated system propositions. The outputs of the study are designed to help ESA understand how the European and Canadian satellite industry can be best supported through its ARTES programme.

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  • Iris Convergence

    Status date: 11 April 2017

    Two approaches were considered in the past for the long term evolution of the safety critical satcom for aviation: Purpose built system with custom air interface (ANTARES) and the incremental evolution of Inmarsat’s system and services (Iris Precursor, Iris Service Evolution). This study helps to converge the two approaches and find synergies.

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  • CABCOM

    Status date: 11 April 2017

    CAN bus has been used in automotive and industrial applications for years in complex systems that require demanding command and control performance. In space systems, the benefits of CAN bus have also been recognized: reducing the number of wires and weight along with lower power consumption and easier testability will result in major cost savings for spacecraft manufacturers. CAN bus is rapidly becoming an on-board standard command and control bus.

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  • AMPT

    Status date: 11 April 2017

    Innovative design of new ITAR free monopropellant 1N thruster developed specifically to out-perform existing flight-proven designs in terms of longevity. Radical use of materials, catalyst loading, nozzle and injector design, filtering and fine particle control, etc. will make this thruster a key player in the 1N chemical thruster market for satellite orbit control systems. Flight Standard Qualification to 44kg throughput was completed in August 2016. Delivery of first flight thruster in September 2016 ensures rapid flight heritage for the MHT-1N with launch planned for June 2017.

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  • LEREA

    Status date: 11 April 2017

    The future generation of communication satellites will use multi-beam antennas providing wide-band two-ways communication applications. Active discrete lens antennas permit generating a multibeam coverage adopting only a single Tx/Rx aperture or two separated Tx and Rx apertures instead of the current solutions based on multi-reflector systems. Reduced volume and maximum EIRP flexibility over the service area are the main advantages of this alternative multibeam antenna. The main criticalities of discrete lens antennas are associated with their mass, physical accommodation, power consumption and thermal control of the high power amplifiers. Reflector antennas exhibit some complementarity with respect to lens antennas: they guarantee a high gain but limited scanning capabilities. Combining a discrete lens with a reflector system would allow reducing the physical size of the lens itself, making it more manageable with respect to the criticalities mentioned above, and at the same time reducing the limitations of reflector antenna systems.

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  • PACS

    Status date: 10 April 2017

    The project aims at developing a testbed in software defined radio (SDR) to prove the feasibility of and measure the performance achievable in practice by the most promising among a set of advanced multiple access schemes for the return link of satellite communications networks

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  • TAG

    Status date: 03 April 2017

    Study defining a concept of use of Thermo-Acoustic Electric Generation for communication satellites, assessing suitable TAG systems, the benefits and constraints of introducing this type of engine into Satcom Satellites, and defining a roadmap for the introduction to market of these engines with the aim of supporting ARTES.

  • Optical RF Distribution Flight Demonstrator (ORFD)

    Status date: 21 March 2017

    This project intends to demonstrate the attractiveness of optical distribution of RF/LO signals in terms of low mass, signal integrity and EMI immunity. A follow-on qualification program will further increase the TRL level of this implementation.

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  • Autonomous Orbit Determination and Station Keeping Control for Competitive Telecom Missions

    Status date: 21 March 2017

    Trade-off on different autonomous orbit-determination solutions including GNSS and optical-based navigation, and a trade-off on different station keeping strategies, to define the global autonomous system best suited for chemical and for hybrid chemical/electrical Telecom platforms on geo-stationary orbit. The chosen solution is based on GNSS and on classical Station Keeping strategy.

  • SatNetCode

    Status date: 18 March 2017

    SatNetCode empowers robust and powerful end-to-end networking over multi-hop integrated satellite networks in potentially difficult mobile scenarios where packet loss and interruptions may occur. By applying adaptive Network Coding – with re-encoding option per network – significant improvements can be obtained over traditional Forward Error Correction approaches. Application areas include aerial, vehicular and maritime users with sources like photos, video and other critical data. The focus is specifically on video over multiple hops.

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  • SB-SAT

    Status date: 08 March 2017

    The SB-SAT (Swift-Broadband for Satellites) spacecraft communications system is designed to enable continuous, near real-time communications between satellite operators and spacecraft in Low Earth Orbit (LEO). The system eliminates the need for expensive new investment in dedicated ground-based communications infrastructure and greatly increases the operational capability of LEO spacecraft.

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  • SHINE (Secure Hybrid In Network caching Environment)

    Status date: 08 March 2017

    An end-to-end secure infrastructure for the delivery of collaborative multimedia services over integrated satellite-terrestrial networks

  • RF COAXIAL CONNECTORS, TNC, VERY HIGH POWER, 50 OHMS

    Status date: 08 March 2017

    Radiall has developed and qualified a new serie of TNC connectors under ARTES 5.1 and 3 contract. Radiall has qualified a complete range of TNC Very High Power connectors. 14 variants have been created and qualified, and three new ESCC detail specifications have been created.

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  • Design Tool for High Performance Antenna Systems with Periodic and Quasi-Periodic Surfaces

    Status date: 07 March 2017

    The objective of the activity is to develop a design tool for RF analysis and optimisation of advanced reflector antenna systems that consist/involve periodic or quasi-periodic surfaces that can either reflect or transmit electromagnetic fields to fulfil certain radiation characteristics when illuminated by an external source.

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  • New Avionics for SATCOM

    Status date: 06 March 2017

    This newly developed generation of avionics for commercial geostationary communications satellites (SATCOM) achieves a significant reduction in cost while at the same time greater flexibility at system and operational level are reached.

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  • RAMSES

    Status date: 24 February 2017

    The RAMSES (Roadmap for Advanced Mobile SatellitE Systems) project has been defined in order to contribute to the definition of roadmaps of new solutions – new technologies, new products – for the successful deployment of Next Generation Mobile Satellite Systems in the 2025 timeframe.

  • GNSS in GTO

    Status date: 22 February 2017

    The Airbus DS GmbH LION Navigator is a multi-GNSS-constellation multi-frequency receiver for spacecraft that is space qualified for operation in low Earth orbits and in-tended for geosynchronous Earth orbits. The goal of the activity is to enlarge the application area of the LION Navigator to launch and early operation phases on transfer up to and including the nominal operation in geosynchronous orbit.

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  • NFG

    Status date: 21 February 2017

    The project comprises investigation on how novel semiconductor technologies (GaN) can be used to meet demanding, future requirements on signal sources. The effort is divided in three consecutive technology steps. This first step include system definition, semiconductor technology trade-off and broadband VCO design including detailed PLL EM unit design. One PLL EM Unit has been built to show function and performance of the VCO.

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  • BEHOP

    Status date: 21 February 2017

    This project represents the basis for enabling satellite systems using beam hopping capabilities to support distributed coverage areas. The coordination between input data, modulator and beam switching payload will be addressed. Furthermore, a receiver capable of operating with bursty DVB-S2X super-framing format 4 waveforms will be designed and implemented.

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  • Network Security on Multi-Spot Beam Broadband Networks for Multicast Based Interactive Systems

    Status date: 20 February 2017

    In this project a secure multicast framework and architecture is defined on top of a multi-spot beam interactive satellite system, including the proposed application scenarios and use cases. A demonstrator is designed and developed to verify and demonstrate the defined secure multicast solution and proposed enhancements. Finally, implementation guidelines and standard evolution recommendation for the secure multicast satellite system are produced.

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  • MTN-CCN2

    Status date: 20 February 2017

    In the main study "Characterization of the Mobile Tracking Needs // ESA AO/1-6669/10/NL/NR" a measurement database was designed, developed and published. The database provides statistics of motion dynamics for mobile satellite terminals. The database (with access to industry residing within ESA member states) supports the design and testing of Satellite Communications On-The-Move (SOTM) tracking systems. The activity included a data gathering campaign and the development and population of a database. In this Contract Change Notice (CCN) standard motion profiles are defined based on the full set of measurements (including new measurements). The motion profiles are included in the GVF-105 standard SOTM test recommendations and their usability and applicability were tested in a pilot test with a commercial SOTM terminal at the Fraunhofer IIS Facility for Over-the-air Research and Testing (FORTE).

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  • HEVC_4K

    Status date: 20 February 2017

    The project developed key technologies for UHD satellite broadcasting systems both for direct-to-home (DTH) services as well as for presenting live events in digital cinemas. It successfully developed and implemented a real-time encoder for High Efficiency Video Coding (HEVC) supporting High Dynamic Range video.

  • KaLQ

    Status date: 17 February 2017

    Through the Artes-34 R&D project “KaLQ” with ESA, Kongsberg Norspace has developed and successfully qualified the two frequency converter units for conversion between Ka- and L-band frequencies. The up- and down-converter units are tailored for use on in a Ka-Band Terminal for Inter Satellite Links.

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  • INSTINCT

    Status date: 31 January 2017

    This project investigates the feasibility of satellite networks integration with terrestrial clouds to dynamically and optimally offer services. It identifies suitable solutions in connection to key satellite capabilities, such as broadcasting/multicasting, large coverage areas, ability to reach remote areas, mobility support, service resilience and flexibility for extending capacity, as well as uniform QoS irrespective of distance to end user.

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  • MARF

    Status date: 30 January 2017

    High power telecom platforms require the deployment of large appendages like solar arrays, antennas or radiators. In many cases their deployment needs to be speed regulated in order to better control their dynamics but also to avoid excessive latching shocks. This activity has been performed to demonstrate the potential of Magneto Rheological fluids in order to provide tuneable speed regulator solutions. An Engineering Model of a self-standing speed regulator unit, based on Magneto Rheological fluid technology, has been produced and tested.

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  • CHVPS

    Status date: 30 January 2017

    The increase of required thrust power will follows the increasing mass and power of future satellite. In the frame of future development, a big challenge consists to develop a high voltage power supply configurable to supply several kind of thrusters.

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  • ACCORD

    Status date: 30 January 2017

    ACCORD specifies a complete platform capable of generating innovative terminals able to automatically reconfigure seamless switching between different air interfaces. This truly innovative approach is based on: Smart router, provides seamless vertical handover selecting the most appropriate network on Quality of Service-based policies; Common Interface, manages satellite and terrestrial air interfaces and their protocols using a fully Software-Defined Radio approach.

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  • 250WkaRC

    Status date: 26 January 2017

    Design, development and test of an engineering model of a wideband and highly efficient radiation-cooled 250 W Ka band space traveling-wave tube.

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  • TxBx2

    Status date: 24 January 2017

    Through the Artes-34 R&D project “Development of 2nd Generation Telemetry and Beacon Transmitter (“TxBx2”) with ESA, Kongsberg Norspace has developed and successfully qualified two new beacon transmitters at C-band and Ku-band. After the completion of the test campaign, the Ku-band unit was rebuilt to a frequency agile Telemetry Transmitter. This EQM is also successfully qualified.

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  • SKYWAN 5G

    Status date: 24 January 2017

    The new SKYWAN 5G is designed for the Next Generation of Satcom. It is THE ONE mesh VSAT network solution with multiple integrated DVB-S2 stars. All data is transmitted reliably in single-hop and time critical data is prioritized avoiding extra delays. The unique hardware design of SKYWAN 5G has already build in the highest flexibility, fits all topologies and enables growth of your network by stacking The ONE modem.

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  • Q/V-Feed

    Status date: 24 January 2017

    The development of a slimline Q/V-band feed system EM suitable for gateway applications in telecoms GEO VHTS systems.

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  • ULRKA

    Status date: 23 January 2017

    Development of a lightweight, low-cost reflector for C, X, Ku and Ka-band applications.

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  • SOTM Standards

    Status date: 23 January 2017

    The activity “Standards Preparation For SOTM Terminals“ is a study to define a common way to specify and verify Satellite On The Move Terminals (SOTM). Currently SOTM terminals are not consistently specified, nor independently verified for a number of key performance criteria. Under these circumstances, it is difficult for service providers, satellite operators, and end users to clearly understand the capabilities of the product being offered without embarking on expensive and lengthy trials. For the SOTM market to continue to grow, obstacles preventing fast and fluid transactions need to be removed, and a clear understanding of product performance needs to be developed. This activity will help move the SOTM market away from the characteristics of a niche market and towards a more established, consumer and manufacturer friendly one.

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  • RSSTP

    Status date: 19 January 2017

    Telecom satellite transponder specifications relating to transmission performances which may be overly stringent, and which could be relaxed, thereby reducing satellite overall cost and schedule.

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  • EASO

    Status date: 18 January 2017

    SPELL (Satellite Procedure Execution Language and Library, https://sourceforge.net/projects/spell-sat/) is a free, open source software package developed by SES in cooperation with GMV. SPELL was conceived in order to automate the execution of satellite procedures. SPELL works on multiple satellite platforms and can be interfaced to multiple ground control systems. From 2011 to 2016, SES planned to launch 12 satellites. In the context of this SES' satellite fleet expansion, there was an inherent need to: • Increase the productivity of satellite controllers; and • Increase the level of standardization and safety in SES' satellite operations.

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  • Next Generation Tactical and Mobile Satcom Systems Study

    Status date: 16 January 2017

    Tactical and mobile satellite has become an increasingly important means of communications for European defence forces. Systems have predominantly been based around the UHF TacSat system, which is quick and easy to use, making it popular with users as a means of providing reliable voice and low rate data communications. However, the limited UHF spectrum and system capacity has meant that users have been looking increasingly to commercial mobile satellite systems to fill the gaps in capability. The Next Generation Tactical and Mobile Satcom Systems Study aims to develop typical user scenarios; identify the capability gaps in current systems; and produce technical (and non-technical) solutions to address these gaps.

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  • Compact and Scalable Ka band Switch Matrix

    Status date: 16 January 2017

    Feasibility of an advanced highly integrated, low mass and cost efficient High Order Scalable Solid State Switch Matrix for use in future Ka-band multibeam payloads, aiming at reaching higher on board capacities, higher number of user beams and even higher number of RF equipment units.

  • Ultra-High Throughput Transmission Through Wideband Ka Transponder

    Status date: 16 January 2017

    The central focus of this project is to develop, integrate, verify and optimise enhanced transmission techniques through testing over wideband satellite transponders, which allow reaching over 1 Gbit/s single carrier per transponder transmission data rates.

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  • Assessment of the socio-economic impact of the ARTES programme

    Status date: 16 January 2017

    Study to estimate the socio-economic impacts of ESA’s Advanced Research in Telecommunications Systems (ARTES) programme in the period 2001-2012. The study follows a mixed-methods approach, which combines qualitative and quantitative techniques to assess various routes to impact and also to arrive at a final estimate of overall economic impact. The study shows that ARTES has enabled major game-changing industrial developments in the past decade and that the economic impact attributable to ARTES is on the order of €19 billion, realised over the past decade. This represents a return of investment of 11 to 1.

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  • ESPRIT

    Status date: 16 January 2017

    During the next two decades, civil Unmanned Aerial Systems (UAS) market is expected to ramp-up exponentially. While UAS integration in non-segregated airspace will start in 2015, regular flights are expected in 2025. ESPRIT aims at identifying and defining the best solution to provide satellite Command & Control communications to UAS when flying in non-segregated airspace.

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  • European Roadmap for Digital OBP Based on Deep Sub-Micron Microelectronics

    Status date: 16 January 2017

    Next generation of flexible payloads will continue to widen towards the on-board processing (OBP) architecture as core of their design. The increasing of the satellite capabilities in term of service and applications demand is pushing the exigency to improve the current way to think and design a SATCOM payload. At European level another mandatory exigency is motivated by the technological non-dependence and competitiveness as stated and stimulated by European Space Agency (ESA) and the European Commission (EC) in the frame of H2020. This is to guarantee not only the non-dependency from products coming from out-side Europe and its affiliate Countries, but also to improve the competitiveness and final product/solutions performances. First step to improve OBP technology towards a Next Generation (NG) is to implement new space components having rad hard characteristics and improved integration scale moving towards deep sub-micron microelectronics (DSM) technology at 65 nm end beyond. The Study has given an outlook on the new space missions and related market interest that are stimulating the DSM as driver for the NG-OBP development. The description starts from an outlook on the state-of-the-art of the OBP technology, watching the main technologies up to now assessed. A view is provided on the relationships between the main actors can be involved in the space DSM and that contribute in the implementation and improvement of this technology. The Study has been concluded providing a summary on the main key functional requirements derived by the provided technology assessment, useful for the future developments and contributing in convincing the satellite market to make the jump towards a new age of the satellite technology. Another item provided in the concluding part of the Study has been the definition of a cost/benefit analysis providing a consistent technology roadmap.

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  • Converters and Local Oscillators for Flexible Payloads

    Status date: 12 January 2017

    The target of the ESA contract. 21425/08 is to design and develop converter and local oscillators for flexible payloads. Thales Alenia Space Italia has designed, manufactured and tested the Engineering Model of the unit verifying the given requirements. As result of this study, Thales Alenia Space is able to propose Ku band Frequency Flexible Down Converters for Flexible Communication Payloads with less units having the same configuration and enhanced flexibility in frequency.

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  • CETB Phase 2

    Status date: 11 January 2017

    The Communication Equipment Test Bed (CETB) phase 2 programme is an evolution of CETB phase-1 which ended in 2013. Phase 1 covered the development of: • TT&C (Telemetry, Telecommand and Control) transceiver • C-band downlink transmitter • High speed data recorder • CCSDS translation node Phase-2 has covered the evolution of the TT&C product to meet market requirements not previously addressed.

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  • 3D-MID4Space

    Status date: 11 January 2017

    3D-MID Technology enables the integration of mechanical, electronic, optical and thermal functions into single parts via selective metallisation offering a high geometric design freedom. This enables the miniaturisation of electronic devices and allows three-dimensional designs to be realised with offer significant reductions in space and weight compared to conventional electronic manufacturing methods.

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  • Advanced Mobility management Protocols (AMP)

    Status date: 10 January 2017

    In future high-capacity multi-beam GEO satellite networks, mobile terminals are subject to relatively frequent beam and gateway handovers with a significant rate of inter-system handovers to be handled by sophisticated IPv6-mobility management solutions. The verification of satcom scenarios on a test bed tailored for heterogeneous mobile networks alongside with the analysis of respective economic impacts are on focus of this activity.

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  • Eurostar 3000 AOCS Mk2 Evolutions

    Status date: 09 January 2017

    Ultimate Eurostar 3000 (E3000) AOCS evolutions for low-thrust transfer and electric station keeping, implemented on full electric telecom satellites: • Accommodation of new gyroscopes and new wheels, • Development and qualification of: o Star tracker-based AOCS for operational and recovery modes, o Management of low-thrust transfer (Electric Orbit Raising = EOR) o Commanding of the robotic arm supporting the electric thrusters in EOR and on-station configuration o Autonomy management with hierarchical Failure Detection Isolation and Recovery (FDIR), commandability and observability optimization adapted to electric transfer.

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  • GaAs Evo1 Solar Arrays Product Family for Spacebus™ 4000C

    Status date: 09 January 2017

    GaAs Triple Junction 30% BOL Solar Array Off-the-Shelf Family for Spacebus Development

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  • Artes 5-2 Low Cost L-Band SSPA

    Status date: 19 December 2016

    A GaN SSPA was developed with the aim of reducing complexity and cost, with increased power (from 15W to 30W), and thus halving the number of operational SSPAs and simplifying payload architecture. The overall SSPA test approach has also been improved with a significant increase in throughput during production realised through streamlining of test stages and optimisation of test algorithms.

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