Funding

This page displays the ARTES Invitation To Tenders (ITTs) which are published on ESA-STAR. If you are looking for a specific element select from the list provided and click on the Apply button to start the search and display the results.

Funding of the individual Prime or subcontractors, for ARTES Core Competitiveness and ARTES Applications activities, is subject to authorisation of the required ARTES budget by the related National Delegations. Therefore, bidding teams are requested to inform their National Delegation(s) of their intention to participate in funded activities already before submitting a proposal.

The official information platform for providing potential bidders all the relevant documentation and details concerning the intended and issued Invitations To Tender (ITTs) for Open Competitions and Direct Negotiations is ESA-STAR - managed and operated by the ESA Procurement Department.

  • BACKGROUND LIGHT AND ATMOSPHERE METROLOGY FOR QUANTUM KEY DISTRIBUTION AT URBAN LOCATIONS (4S SAGA)

    Development of tools and hardware and the execution of a measurement campaign for background light and atmosphere conditions for Quantum Key Distribution (QKD) at urban location (major cities and metropolitan areas) under ARTES 4.0 Space Systems for Safety and Security (4S) Strategic Programme Line. These measurement results are an important check point to validate the design of the SAGA system. The background light and atmosphere metrology ac…

  • POWER MODULE FOR AUTONOMOUS SATELLITES (ARTES AT 4F.095)

    The objective of the activity is to design, manufacture and test a power module that will be integrated in an autonomous spacecraftarchitecture.Targeted Improvements:Increase the level of onboard autonomy by 50% at overall platform level.Description: Current satellite operations require human intervention from ground, resulting in considerable inefficiencies and dependencies on communication window frequency, latency, and available resources,…

  • RAPID AND FLEXIBLE END-TO-END MANUFACTURING PROCESS FOR COMPLEX-SHAPED COMPOSITE REFLECTOR ANTENNA (ARTES 4.0 AT 5B.226)

    The objective of the activity is to develop rapid and flexible advanced manufacturing techniques, with a full digital workflow, forhigh volume production of complex-shaped composite reflector antennas from 1 to 3.5 metres in diameter.Targeted Improvements:Reduction in composite reflector manufacturing time by a factor of five in comparison to standard metallic mould processes.Description:Today, the manufacturing lead time of reflector antennas…

  • MULTI-PLATFORM DUAL BAND CONFIGURABLE POWER AMPLIFIER FOR AVIONIC TERMINALS (ARTES AT 7C.052) (ON DELEGATION REQUEST)

    Objective: The objective of the activity is to develop, manufacture and test a breadboard of a L- and C-band configurable power amplifier to enable dual band operation of avionic terminals. It shall demonstrate 200W peak power per channel and a 10dB dynamic rangewith a constant average power added efficiency of at least 50% for both bands, without compromising linearity performance. The breadboard shall include driver, main and peak amplifier,…

  • 500 AMPERE CLASS POWER UNIT FOR ONBOARD PAYLOAD SIGNAL PROCESSING HARDWARE IN COMMUNICATION SATELLITES (ARTES AT 5C.516)

    The objective of this activity is to design, manufacture and test a 500A class power unit capable of supplying DC power for both large on-board and AI processors for use in communication satellites.Targeted Improvements: Improved current supply capability of voltage regulators by a factor of ten enabling the use of high performance AI processors (GPUs and TPUs) in future telecom satellites.Description: Artificial Intelligence (AI) processors,…

  • SYSTEM ARCHITECTURE AND WAVEFORM FOR AERONAUTICAL MOBILE-SATELLITE ROUTE SAFETY AND SECURITY SERVICES IN C-BAND ( ARTES 4.0 SPL 4S 3A.198)

    The objective of this activity is to design, develop and validate a system architecture and suitable waveform for an Aeronautical Mobile-Satellite (Route) Services (AMS(R)S) constellation in C-band for safety and security services.

  • MAGNETIC BEARING SYSTEMS FOR HIGH-SPEED ROTARY MECHANISMS (ARTES 4.0 AT 4E.092)

    Objective: The objective of the activity is to design, manufacture and test a magnetic bearing system for high-speed rotary mechanisms in telecommunication spacecraft applications (e.g. reaction wheels or thermal control pumps and compressors). Targeted Improvements:- Increase rotation speed by a factor of 2 (resulting in higher angular momentum capability). - Increase lifetime by a factor of 2 (due to contact-less bearings and no lubrication)…

  • SPARSE TRANSMIT KA-BAND ACTIVE PHASED ARRAYS FOR GROUND TERMINALS CONNECTED WITH SATELLITES IN DIFFERENT ORBITS (ARTES AT 7A.077)

    The objective of this activity is to develop and test a Ka-band sparse active transmit antenna breadboard and associated beamforming network for ground terminals to be connected with satellites in orbits ranging from geostationary orbits to low earth orbit orbits. Targeted Improvements: - 25% reduction in the number of active controls.- 5% increase in the DC-to-RF power efficiency at antenna level, due to the reduced exploitation of amplitude…

  • SMALLSAT PLATFORM WITH SELF-TRANSFER CAPABILITY INTO GEOSYNCHRONOUS ORBIT (ARTES AT 3E.001) (ON DELEGATION REQUEST)

    The objective of this activity is to develop radiation tolerant platform technologies and semi-autonomous orbit transfer capabilityfor small satellite platforms. An experimental small satellite will be designed, manufactured and launched. The satellite will feature the platform technologies developed as well as a simple telecommunication payload allowing experiments during orbit raising to GEO as well as in GSO. Targeted Improvements: Enabling…

  • ION THRUSTER GRID IMPEDANCE MEASUREMENT DEVICE FOR IN-FLIGHT THRUSTER HEALTH MONITORING (ARTES AT 4B.182)

    The objective of this activity is to extend the thruster lifetime and optimise the operating point of the thruster and to develop afinite element model of the grids system together with the plasma in between to allow health checks.Targeted Improvements:- 20%increase in thruster lifetime.- 20% decrease of grid thruster failure probability (erosion).Description: Telecom platforms couldbenefit from gridded ion thrusters in the near future, but c…

  • HIGHLY INTEGRATED TRANSMIT AND RECEIVE DIRECT RADIATING ANTENNA ARRAY BASED ON MM-WAVE SILICON TECHNOLOGIES AND PACKAGING (ARTES AT 5B.241)

    The objective of the activity is to develop a highly integrated, scalable Ku or Ka-band TX/RX direct radiating array, for versatileconnectivity missions in low earth orbit. Critical breadboarding will be carried out, levering the advances in Mm-wave silicon technologies and advanced packaging techniques to achieve a high degree of integration. Targeted Improvements: Enabling highly integrated combined transmit and receive active antenna with a…

  • SINGLE-CHIP 71-86 GHZ TRANSCEIVER RFIC FOR AERONAUTICAL SATCOM APPLICATIONS (ARTES AT 6A.074) (ON DELEGATION REQUEST)

    The objective of the activity is to design, manufacture and test an integrated W-band transceiver Radio Frequency Integrated Circuit (RFIC) configurable as transmitter and receiver covering the 71-86 GHz band for aeronautical satcom applications. Targeted Improvements: Enable satellite aeronautical broadband services in W-band. Description: The maturity of Silicon technologies allows for the implementation of multifunctional and reconfigurable…

  • SINGLE-PIECE-PART W-BAND PHASED ARRAY ANTENNA INCLUDING THE PASSIVE RF FRONT-END (ARTES AT 5B.239)

    The objective of this activity is to design, manufacture and test a W-band/E-band phased array antenna including the passive RF front-end taking advantage of additive and hybrid manufacturing techniques in order to reduce its complexity and mass compared to conventional subtractive techniquesTargeted Improvements: 30% mass reduction, removing screws and assembly interfaces.Description: With the multiplication of broadband communication satelli…

  • ASIC/FPGA WITH 112 GBPS OPTICAL I/OS (ARTES 4.0 SL SPL 5C.480)

    The objective of this activity is to develop the technology step needed to enable the use of optical interconnects at speeds of up to 112 Gbps. This should be demonstrated through testing of an integrated digital signal functions (ASIC and FPGAs) with the developed electro-optic transceiver photonic integrated circuits that form the optical I/Os to replace traditional electrical I/O.Targeted Improvements:Increase the data rate throughput up to…

  • MULTIFUNCTIONAL HINGE FOR LARGE ON-BOARD DIRECT SATELLITE-TO-DEVICE ACTIVE ANTENNA ARRAYS (ARTES 4.0 SPL 5G/6G 4E.093)

    The objective of the activity is to develop and test a multifunctional hinge technology to accommodate a large multi panel active antenna array on a spacecraft platform, with integrated sensing to avoid adverse local deflections due to spacecraft dynamics.Targeted Improvements:Enabling technology for very large active antennas with disperse panels to be accommodated on a spacecraft platformfor future 5G/6G (direct to handheld) satellitesDescri…

  • SPACEBORNE W-BAND HIGH POWER TRAVELLING WAVE TUBE (ARTES AT 5C.486) (ON DELEGATION REQUEST)

    The objective of this activity is to design, develop and test a breadboard of high-power W-band travelling wave tube (TWT) to meet the requirements of Very High Throughput Satellites.Targeted Improvements:Enable a European source of W-band TWT with 5 GHz instantaneous bandwidth, 100 W power output and at least 30% efficiency.Description:High Throughput Satellites (HTS) and Very High Throughput Satellites (VHTS) already use Q/V band frequencies…

  • VERY LOW EARTH ORBIT SYSTEM SIMULATOR FOR DIRECT SATELLITE-TO-DEVICE 5G/6G COMMUNICATIONS (ARTES 4.0 SPL 5G/6G 3F.019)

    Objective: The objective of the activity is to develop and test a system simulator testbed capable of modelling and assessing the performance of communication satellite constellations operating in Very Low Earth Orbit (VLEO). This includes the assessment of the emerging waveforms (5G NTN, European Protected Waveform).Targeted Improvements: Enable the design and assess the constellation system performance of communication satellites operating i…

  • SATELLITE COMMUNICATION TEST-BED ON-BOARD THE INTERNATIONAL SPACE STATION (ARTES AT 3A.118) (ON DELEGATION REQUEST)

    Objective: The objective of this activity is to develop, deploy and operate a flexible software-defined radio communication testbedwith a frequency flexible RF front end on the International Space Station, supporting a wide range of frequencies up to Q/V band addressing 5G, signal processing and advanced techniques. Targeted Improvements: Enabling innovative and fast developments of future satcom applications from UHF to Q/V band that are diff…

  • SPIN-IN OF SLIPRING TECHNOLOGY FOR SATCOM APPLICATIONS (ARTES AT 4E.096)

    The objective of the activity is to select an off the shelf European slipring technology for terrestrial applications and demonstrate its suitability for Satcom applicationTargeted Improvements: Improving by 20% of power density, lifetime, mass, volume, and lead time.Description: Solar Array Drive Mechanism (SADM) require complex slip-ring technology often leading to long delivery times. However, slipring technologies for terrestrial applicati…

  • RECONFIGURABLE ANTENNAS FOR MOBILE TERMINALS BASED ON ACTIVE ACTUATORS (ARTES 4.0 AT 7C.080)

    The objective of the activity is to design, manufacture and test a Ku- or Ka-band transmit or receive antenna based on reconfigurable actuators for large mobile terminals connected to Low Earth Orbit (LEO) satellites.Targeted Improvements:Enabling reconfigurable terminal antennas with scan angles up to 50-60 degrees exploiting active actuators like pin or varactor diodes, MEMS and other possible actuators with an overall antenna thickness belo…

  • ON-CHIP ACTIVE RECONFIGURABLE FILTERS FOR 5G PHASED ARRAY ANTENNAS (ARTES 4.0 SPL 5G/6G 7A.076)

    The objective is to develop and test a Ku or Ka band transparent phased array antenna to provide broadband connectivity on board cars. Targeted Improvements: Develop a new class of phased array antennas for cars able to guarantee a seamless broadband connectivitywith LEO satellites. Description: There is today a significant interest to provide broadband connectivity to cars. This request is associated to the need to guarantee emergency service…

  • IMPLEMENTATION OF SOFTWARE MITIGATION SOLUTIONS FOR RADIATION-INDUCED SINGLE EVENT EFFECTS (ARTES 4.0 AT 5C.490) - RE-ISSUE OF ITT 1-11734

    The objective of the activity is to de-risk software mitigation techniques for radiation effects on a family of high-performance processors embedded in System on Chip (SoC) components. The activity will identify, on one or more processors of interest for the industry, radiation-induced failure modes and will implement appropriate software mitigation techniques with reuse or development of small FPGA IPs if needed. Targeted Improvements: Enable…

  • SPATIALLY COMBINED 40 W - 60 W Q-BAND SOLID STATE POWER AMPLIFIER (ARTES 4.0 AT 5C.494)

    The objective of this activity is to develop, manufacture and test a highly efficient Q-band spatial power divider and combiner forapplication in Q-band Solid State Power Amplifiers (SSPA). Experimental performance verification shall be carried out on a 40 - 60 W (nominal operating point) Q-band SSPA breadboard. Targeted Improvements: Improved power added efficiency of 5 - 10% of Q-band SSPAs in comparison to the state of the art. Description:…

  • DEMISABILITY OF OPTICAL COMMUNICATION TERMINALS FOR SATCOM CONSTELLATIONS IN LEO (ARTES 4.0 SL SPL 5A.081)

    Objective:The key objective of this activity will be the investigation of the demise behaviour of different optical communicationterminals for current and future applications on-board satcom platforms in LEO (e.g. future constellations) and therefore the development of breadboard of the design for demise solutions and technologies identified to reduce the on-ground casualty risks associated with these elements.Targeted Improvements:Reduce by a…

  • SOFTWARE SIMULATOR FOR AIR/SPACE TRAFFIC MANAGEMENT VIA SATELLITE FOR HYPERSONIC SPACE PLANES (ARTES 4.0 4S SPL 3A.155 / 4S.013) - EXPRO+

    Objective: The objective of the activity is to design and develop a physical layer simulator in order to assess the communication needs, and develop a system concept to support air/space traffic management considering emerging transport means such as hypersonic space planes. Targeted Improvements: Enabling communications for a future European Air/Space Traffic Management System in support of hypersonic space planes. Performance improvement wit…