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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.
KA-BAND TRANSMIT SPARSE ACTIVE PHASED ARRAY AND BEAMFORMING NETWORKS FOR NGSO USER LINKS (ARTES AT 5B.240)
The objective of this activity is to design, manufacture and test a partial RF breadboard of a transmit Ka-band, active phased array antenna and associated beamforming network for user links NGSO, exploiting irregular layouts for the radiating elements and beamforming networks.Targeted Improvements: In comparison to a standard, fully populated array:- 25% reduction in the number of active controls,- 5% increase in the DC to RF power efficiency…
ATMOSPHERIC TURBULENCE EFFECT MITIGATION BY SECONDARY MIRROR ACTUATION (ARTES 4.0 SL SPL 6C.020)
Objective: The objective of this activity is to simplify optical feeder links systems in Optical Ground Stations by replacing the secondary mirror with an active (deformable) one and to demonstrate the improvement in transmission budget and complexity. Targeted Improvements: 30% increased optical throughput in optical communication ground stations. 20% reduction of complexity in adaptive optics and beam pre-distortion in feeder-link systems. R…
SECURITY ASSESSMENT, TESTING AND VALIDATION CAPABILITY FOR INNOVATIVE SECURE COMMUNICATIONS AND QUANTUM TECHNOLOGIES (ARTES 4.0 4S SPL 3D.018) RE-ISSUE
The objectives of the activity are to identify the needs and requirements for new security assessment capabilities for satcom systems and their components, define related architectural solutions and develop prototypes of the main components of these capabilities.Targeted Improvements: Enabling testing, verification and validation of advanced technologies in the domain of cybersecurity, modern telecom and quantum security (Quantum Key Distribut…
ZERO-TRUST ARCHITECTURE FOR LOW EARTH ORBIT REGENERATIVE PAYLOADS ( ARTES 4.0 SPL 4S 3D.029)
The objective of this activity is to design+ implement+ and validate a zero-trust architecture for a Low Earth Orbit regenerative 5G gNodeB+ that mitigates the security risks specific to 5G Non-Terrestrial Networks.
IN ORBIT EXPERIMENT OF AUTONOMOUS DEPLOYMENT AND EARLY OPERATIONS FOR TELECOM CONSTELLATION SATELLITES (ARTES AT 3E.024) (ON DELEGATION REQUEST)
The objective of this activity is to design and perform an in-orbit experiment investigating autonomous deployment and early operations for telecom constellation satellites. This includes the development of command and data-handling hardware as well as AI/ML based operational algorithms developed on-ground.Targeted Improvements: Increase of onboard autonomy by 50% (i.e. include the key number of autonomous functions), including attitude acquis…
MASS MEMORY UNIT WITH 100 GIGABIT PER SECOND WRITE RATE CLASS FOR LOW EARTH ORBIT COMMUNICATION APPLICATIONS (ARTES AT 5C.498) (ON DELEGATION REQUEST)
The objective of this activity is to design, manufacture and test a memory unit breadboard offering interface port and memory read and write speeds at 100 GigaBit per second and a capacity of at least 3 TeraBits for interconnected constellation telecommunication systems. Targeted Improvements: Improvement of the write speed by a factor of 10 compared to FLASH-based mass memories. Description:Future Low Earth Orbit (LEO) constellations with hig…
HIGH IMPULSE ARGON ELECTRIC THRUSTER (ARTES AT 4B.181)
The objective of the activity is to design, manufacture and test an electric thruster using Argon propellant, compatible with the long lifetime and high total impulse requirements of telecommunication satellites in GEO and for constellations.Targeted Improvements:- Novel capability to operate with Argon propellant not existing today.- Improved lifetime and Total Impulse per kW(N.s/kW) by a factor of 2.- Decreased complexity of the thruster arc…
DRAG AND ATOMIC OXYGEN RESISTANT CARBON FIBRE REINFORCED POLYMER FOR VERY LOW EARTH ORBIT TELECOM SATELLITES (ARTES AT 4A.092) (ON DELEGATION REQUEST)
The objective of the activity is to develop and test a coating material (e.g. for substrates such as carbon fibre reinforced polymer, polymers, etc) with improved atomic oxygen and drag resistance to be used on the external satellite surfaces for very low Earth orbit applicationsTargeted Improvements:- Enabling technology not existing today; allowing telecommunication satellites with conventional construction materials in much lower orbits tha…
ARTES 4.0 SPL 4S 3A.199 RADIO RESOURCE MANAGEMENT TECHNIQUES FOR JAMMING MITIGATION IN NGSO CONSTELLATIONS
The objective of the activity is to design, develop and test jamming mitigation strategies for NGSO broadband secure systems based on adaptive radio resource management algorithms.
SOLAR ARRAY WITH LATCHED SHALLOW CURVED SURFACE FOR IMPROVED DEPLOYED STIFFNESS (ARTES AT 4F.161) (ON DELEGATION REQUEST)
The objective of the activity is to develop, manufacture and test a latch to enhance the deployed stiffness of an existing array, by means of a slight repositioning of panels. Targeted Improvements: Increase the frequencies of the deployed array by 30%.Description: Most telecommunication solar arrays comprise in-line panels, arranged in a row. Some include lateral panels, forming a cross configuration. In the case of the latter, the frequency…
ONBOARD DATA HANDLING SUB-SYSTEM FOR AUTONOMOUS SATELLITES (ARTES AT 4G.044)
The objective is to develop an onboard data handling architecture capable of autonomously acquiring, processing and interpreting housekeeping and telemetry data and taking the required actions without ground intervention. The activity will develop a data handlingsub-system demonstrator to validate the intelligent functionalities, including prognostic and health management (PHM) capabilitiesTargeted Improvements: Enabling technology development…
L-BAND GALLIUM NITRIDE LOW NOISE AMPLIFIER-BASED RF FRONT-END (ARTES AT 5C.465) (ON DELEGATION REQUEST)
The objective of the activity is to design a compact L-band RF front-end for telecom applications which is based on a GaN Low NoiseAmplifier (LNA). A breadboard of a GaN microwave monolithic integrated circuit will be developed and tested. The RF front-end including the filtering function shall be modelled.Targeted Improvements: up to 30% mass and volume saving of the RF front-end (LNA and filtering) and 20 dB improvement of the LNA dynamic ra…
10W PER MM CLASS THERMALLY ENHANCED HIGH EFFICIENCY MICROWAVE POWER AMPLIFIERS (ARTES 4.0 AT 5C.491) (RE-ISSUE)
The objective of this activity is to design, manufacture and test a breadboard of a high-power amplifier in Ku-band or above with 10 W/mm class of power density in continuous wave operation. The selected manufacturing process will allow a smaller chip size with reduced junction temperature, reduced thermal memory effects and improved efficiency.Targeted Improvements:- 3-5 times improvementin power density.- Junction temperature reduction of te…
EUROPEAN CHIP INDUCTOR FOR POINT OF LOAD CONVERTERS IN TELECOMMUNICATION SATELLITES (ARTES 4.0 AT 5C.499)
The objective of the activity is to design, manufacture and test surface mount chip inductors enabling low voltage (down to 0.8 V range) stability, fast transient response, high-speed switching capability and efficient power conversion of point of load(POL) converters, as needed for next generation digital integrated circuits in telecommunication satellites.Targeted Improvements:- Enablinga European source.- 20% mass and volume reduction and 2…
POWER EFFICIENT DESIGN OF RADIO FREQUENCY PAYLOAD ALGORITHMS ON SYSTEM ON CHIP (ARTES AT 5C.513)
The objective of the activity is to identify and benchmark power efficient radio frequency algorithms on complex System on Chip (SoC) devices. Power efficient algorithms for at least two applications case (e.g. beamforming, decoding/encoding, neural networks...) will be designed, developed and tested and compared to programmable logic only implementation.Targeted Improvements: 50% reductionpower consumption for radio frequency algorithms with…
BREADBOARDING OF CRITICAL TECHNOLOGIES FOR A MULTI-BEAM SATELLITE RECEIVER FOR AIRCRAFT MODE-S SIGNALS (ARTES 4.0 4S SPL 5A.082) (ON DELEGATION REQUEST)
The objective of the activity is to design, develop and test payload technologies compliant with multi-beam receivers for satellite-based air traffic surveillance. Critical breadboarding will be carried out to demonstrate the concept suitable for use on small satellites in LEO or MEO. Targeted Improvements: 50% reduced payload power consumption, mass and volume compared to current technology.Increase the probability of message detection by a f…
DIGITAL TWIN FOR ON-ORBIT ASSEMBLY AND MANUFACTURING OF VERY LARGE ANTENNAS (ARTES AT 5B.235)
The objective of the activity is to develop and test a digital-twin for on-orbit assembly and manufacturing of antennas up to 30-50metres diameter. An end-to-end manufacturing process will be selected and guidance, navigation and control techniques for assembly and manufacturing on-orbit will be developed. A simple large reflector antenna will be designed, and assembly and manufacturing will be evaluated with the developed digital twin.Targete…
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…
LUNAR LASER COMMUNICATION TERMINAL (ARTES 4.0 SL SPL 5G.045)
Objective: The objective of the activity is to first design a Laser Communication Terminal (LCT) concept suitable for communicationover lunar distances. In a second step, the activity will develop an engineering model of a CCSDS compatible transceiver with critical functions including coding, synchronisation, and modulation. Targeted Improvements: Enabling a European or Canadian lunar communication terminal operating with a data rate one order…
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,…
ARTES 4.0 SPL 4S 7B.077 - EMERGENCY LIGHTS FOR CARS IN DISTRESS WITH INTEGRATED TERRESTRIAL AND SATELLITE CONNECTIVITY (ON DELEGATION REQUEST)
The objective of the activity is to develop and test a prototype of the emergency car light device with direct to satellite communication capability in an emulated environment in laboratory.Procurement Policy: C(1) = Activity restricted to non-prime contractors(incl. SMEs). For additional information please go to:…
ACCELEROMETER FOR DRAG COMPENSATION IN VERY LOW EARTH ORBIT (ARTES AT 4C.069) (ON DELEGATION REQUEST)
The objective of the activity is to design, manufacture and test an accelerometer for drag compensation in Very Low Earth Orbit (VLEO). Targeted Improvements: - Enabling real time compensation of drag by the propulsion system. - Miniaturisation of instrument by a factor 10 compared to existing payload grade accelerometers. - Increase accuracy by factor 10 compared to existing accelerometers used for orbital control.Description: While intere…
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)…
DISTINCT TRANSMIT AND RECEIVE SATELLITE SYSTEM FOR SIMULTANEOUS TWO-WAY LOW DATA RATE COMMUNICATION SERVICES (ARTES AT 3A.202)
The objective of the activity is to design a system concept based on distinct transmit-only and receive-only satellites for the user link. The goal is to enable at the system level simultaneous two-way low data rate communication services such as Internet of Things, messaging, and VDES operating in frequency range from VHF to C-band. The system concept will be implemented and tested in an end-to-end system testbed. This includes the user termi…