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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.
BUFFERBLOAT FREE AND CONGESTION RESILIENT SATCOM NETWORKS (ARTES AT 6B.129)
The objective of this activity is to design, implement and test active queuing management and packet scheduling techniques at the user terminals and ground equipment, so that the SATCOM network continues to provide seamlessly an acceptable throughput and latency to users under any congestion situation.Targeted Improvements:- Enabling a responsive and fair SATCOM network in any traffic andresources availability situation.- Keeping the addition…
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…
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…
COMPACT VHF-BAND DIPLEXER FOR SMALL SATELLITE VHF DATA EXCHANGE PAYLOADS (ARTES AT 5E.030)
The objective of the activity is to design, manufacture and test a compact transmit-receive diplexer engineering model with high isolation, low loss and power handling as required for full duplex VHF data exchange payloads.Targeted Improvements: Enabling technology for full duplex VHF data exchange system (VDES) payloads on small satellite platforms.Description: The World Radiocommunication Conference in 2019 allocated maritime VHF frequencies…
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…
MULTIFREQUENCY TRANSMIT ACTIVE PHASED ARRAYS FOR GROUND TERMINALS CONNECTED WITH MULTI-ORBIT NON GEOSTATIONARY ORBIT SATELLITES (ARTES AT 7A.078)
The objective of this activity is to design, develop and test enabling technologies for multi frequency transmit active antenna. This will include antenna radiating elements, beamforming techniques and active elements designed to cover Ku and Ka transmit frequency bands for ground terminals connected to non-geostationary multi-orbit satellites.Targeted Improvements: - Mass and size reduction by 30% by sharing components between frequency bands…
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…
PREDICTIVE QUALITY OF SERVICE (QOS) PROTOCOL FOR NON-TERRESTRIAL NETWORKS IN SUPPORT OF AUTOMOTIVE SERVICES (ARTES 4.0 SPL 5G/6G 3F.023)
Objective:This objective of this activity is to develop and test an extended protocol to address the support of predictive Qualityof Service (QoS) in Non-Terrestrial Networks (NTNs). The activity will also undertake the necessary investigation and selection of data-driven algorithms to automate predictive QoS in NTN.Targeted Improvements:Features enhancement to align NTN solutions in an integrated NTN/TN ecosystem in support to automotive serv…
LOW COMPLEXITY SOLAR CELLS FOR HIGH VOLUME PRODUCTION (ARTES AT 4F.170)
The objective of this activity is to develop, manufacture and test new solar cells with new structures, new processes that will increase the throughput.Targeted Improvements: Doubling the production throughput by the introduction of innovative processes with anew solar cell designDescription: Currently the demand of highly efficient solar cells is exceeding the supply and requires to bemuch more competitive. Simplified manufacturing processes…
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…
MACHINE LEARNING TECHNIQUES FOR DATA RATE REDUCTION (ARTES AT 7B.079)
The objective of this activity is to design, implement and test Machine Learning (ML) and Artificial Intelligence (AI) based data rate reduction techniques for ground terminals. A testbed will be developed to assess performance savings in terms of throughput, complexity and power consumption.Targeted Improvements: Decrease the transmitted data rate by at least 40% for specific applicationsDescription: Many types of data transmissions and recep…
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,…
NUTATION BASED FINE TRACKING SYSTEM FOR SPACE OPTICAL COMMUNICATION TERMINALS (ARTES 4.0 SL SPL 5F.049)
Objective: The objective of the activity is to develop a fine tracking system with reduced complexity and size. The fine tracking of optical communication terminals shall be based on Rx-fibre or Rxbeam nutation for probing the point spread function at the focal plane and will replace the need for a tracking sensor. Targeted Improvements: Reduce the size weight, power and cost of space opticalcommunication terminals by 30%. Description: Nutatio…
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:…
BEAMFORMING BASED ON LOW-RESOLUTION, LOW POWER CONSUMPTION ANALOGUE TO DIGITAL CONVERTERS (ARTES AT 5C.512) (ON DELEGATION REQUEST)
The objective of the activity is to develop a beamforming concept based on low resolution and low power consumption Components of The Shelf (COTS) Analogue-to-Digital Converters (ADC). The developed concept will be implemented and tested in a combined software and hardware testbed. Targeted improvements: Improved energy efficiency by >50% thanks to the use of low resolution and low power ADC when compared to 10-12 bit resolution ADCs. Descr…
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)…
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,…
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…
ADAPTIVE THERMAL CONTROL OF TELECOM SATELLITES (ARTES 4.0 AT 4D.082) (RE-ISSUE)
The objective of the activity is to develop and test a breadboard of an electrophoretic panel enabling adaptive thermal control on telecommunication spacecraft. Targeted Improvements:-Enabling technology to allow adaptive control of radiative surfaces.-Reduction in heater power of 40% and in radiator size of 30%. Description: Traditional thermal design balances emissivity and absorption parameters based on surface materials and/or coatings sel…
IN-ORBIT EXPERIMENT OF A VLEO SATELLITE TO ENABLE PRECISE ORBITAL MODELLING AND SYSTEM SIZING (ARTES AT 3E.026) (ON DELEGATION REQUEST)
The objective of the activity is to develop high fidelity models to allow the mission design of satcom constellations in VLEO. An in-orbit experiment will be designed and manufactured to measure key geographically and time dependent atmospheric parameters (density, radiation, ionospheric, chemical composition etc..) as well as satellite flight parameters (including drag, solar cells efficiency, etc..). These measurements will enable the precis…
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,…
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…
PRINTED CIRCUIT BOARD TECHNOLOGY FOR AUTOMOTIVE CONFORMAL ANTENNAS (ARTES 4.0 AT 7C.083)
The objective of the activity is to investigate, develop and test conformal Printed Circuit Board (PCB) technology using a novel approach, such as additive manufacturing to "print" the antenna for the automotive market. Targeted Improvements: Enabling conformal board of patches with distribution feed and integration of amplifiers on the reverse side, able to follow the shape of a car roof. Description: Conventional PCB technology is…
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…
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…