In this project a 3-axis mechanically tracking antenna has been developed by SpaceCom A/S. Main design goals are: State-of-the-art performance when exposed to tough vibration/shock specifications and high tracking accuracy (<0.2°) in rough seas, at a competitive price.

Extended lifetime normally-closed high pressure valve for orbital propulsion systems

This project incorporates the implementation of DVB-RCS2 in the SatLink system, in embedded SW and FW for the hardware units developed in another ARTES3-4 project, and as SW on SatLink NMS and NCC.

The objective of this activity is to survey existing radome designs and identify relevant performance characteristics applicable to radomes used by mobile satellite ground user terminal antennas operating in Ku-band and Ka-band in different mobile environments.

The objective of the MIGNON project is to develop and evaluate Ka-band surface mountable miniaturized cavity filters realized in multilayer micro-machined technolog

The On-board Signal Processing platform serves as a common core for a product family and is built around a highly integrated commercial SRAM-based FPGA. Each product within the family is customized by the development of mission- or market-specific signal processing firmware and RF front-ends.

T6 High Power Electric Propulsion System (HPEPS) is a flexible and modular 5kW-class EP system to provide for geostationary communication satellites (GEO comsats) high Specific Impulse electric propulsion for orbit raising; station keeping, comsat GEO repositioning (as required) and satellite disposal to graveyard orbit at end of mission.

The Damped Ultra-light Deployment Mechanism - a hinge consisting out of elastic collapsible CFRP blades and a damping device- is developed to deploy a wide range of structures, smoothly with a minimal end shock based on a Shape Memory Alloy spring. The ultra-lightweight design combined with high stiffness, thermal stability and low power consumption is the key in this product.

ComDev Europe (traded as Honeywell) are seeking to take advantage of the configurability and weight saving of software defined radio in a new high speed X-band downlink capability. Balancing spectrum, ground station availability and the high-speed modulation currently available, we are developing a low mass, power and volume system with reduced complexity in a dependable product, targeting the ever-growing data requirements of future missions.

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 approaches. Application areas include aerial, vehicular and maritime users with sources like video and other critical data. The focus is specifically on video over multiple hops.

Based on HPS/INVENT CFRP technologies a 2.4 m Q/V band reflector with highest accuracy was designed, manufactured and tested. The design concept proved to be applicable for multi-beam telecom application. With a frequency band of 37.5 GHz to 51.4 GHz this is the next step for a Terabit satellite to provide high-speed internet.

This study examines various technical solutions and associated technologies for design compact feed network from L-band to C-band and validates the most promising by manufacturing and testing a representative EM of critical parts of the network. Activities were focused on the feed network to have a significant number of beams while maintaining acceptable mass and dimensions of the feed network.

This project aims to develop an electronic scanning multibeam antenna ground station combining gateway and TT&C services in Ka band for LEO and MEO satellite megaconstellations.

Delta Development and qualification of PCU derived from latest PCU generation to address Chinese market demand

Experiments of optical multi aperture up-links between OGS and ARTEMIS satellite executed in the past did not show the expected effects due to TX diversity.

The application of high temperature adhesives and potting materials becomes more challenging when not only a very good thermal endurance is required, but also where the application is in high voltage ranges. For Telecom missions, this applies especially for travelling wave tubes, power transfer applications e.g slip rings, electrical propulsion power supplies and power connectors and lines.
In this activity, adhesives with enhanced thermal stability and insulation properties for high voltage applications have been selected and validated.

The aim of the project is to develop a new generation of Command Receiver to offer improved performances and flexibility to operators and prime contractors. This new product implements a CDMA demodulation mode increasing significantly the immunity against interferers.

CESI project was aimed at developing of high efficiency large area solar cells from 6” Ge wafers.
Large area devices lead to a significant benefit at space power generators level, as they reduce, for a given power, the panel complexity saving space and weight. CTJ30-CLASS is the building-block for the future generations of PVAs, especially for high power demanding missions.

The RAD-EDFA-HP programme covers the development of high power optical fibre amplifiers (OFAs) for space laser communication.
Amplifiers are developed for C-band operation with 30dBm and 35dBm output power to cover the applications of LEO to ground, intra and inter satellite links (LEO to GEO and GEO to GEO).

Arralis have delivered a Ka Band Transceiver Chipset to the European Space Agency for space communications applications.

The Low Rate VSAT SCADA Network development has resulted in a unique low-data rate all-in-one DVB-S2/RCS integrated terminal optimized for Industrial IoT applications.

The activities under the SAAF project address the ancillary functionalities and auto-test capabilities that coupled with a power producing Solar Array Simulator (SAS) would provide the full simulation and verification capability of the power and dynamic aspects of a spacecraft Solar Array.

Development of the next generation UHF/VHF Antenna Systems

The SKATE project is focused on the development and test of a proof-of-concept of a highly integrated Ka-band low cost BFN/RF front-end using SiGe MMIC with a high number of control nodes on chip for user mobile terminal using. The final aim is to achieve a very significant cost reduction of the array and hence the user terminal recurrent cost.

AR4Telecom main goal was the development and testing of SW/HW tools which could bring the benefits of Augmented Reality tech into the realm of AIT/V work-related processes, focusing on the increasing of productivity while reducing human related error instances. LusoSpace (PT) and ENEA (RO) joined forces to build this solution.

SATis5 aims to build a large-scale real-time live end-to-end 5G integrated satellite terrestrial network proof-of-concept testbed. The demonstrator testbed implements, deploys and evaluates an integrated satellite-terrestrial 5G network, showcasing the benefits of the satellite integration with the terrestrial infrastructures as part of a comprehensive communication system.

Relevant satellite use cases for 5G to be demonstrated in SATis5 include enhanced mobile broadband (eMBB) and massive machine type communications (mMTC). The SATis5 demonstrator covers live, over-the-air GEO and MEO satellite field demonstrations in addition to laboratory emulations and simulations in a federation of testbeds. The demonstrator is an open federation of resources that can integrate or incorporate additional resources and testbeds in the future providing a more diverse set of experiments and demonstrations.

Design and development of a high gain deployable antenna dedicated to small satellites (3 to 28 kg range). The overall architecture is simplified as much as possible to reduce any possible source of defective actuation/deployment.

Ferrite Phase shifter driver unit for Flexible antenna applications.

Tight frequency reuse, e.g., beyond a 4-color scheme to increase a multi-beam satellite system’s capacity could make signal detection ‘interference-limited’, where conventional interference suppressing techniques would be ineffective, requiring rather some sophisticated/novel techniques, e.g., those exploiting interfering signals, to revive the overly degraded desired signals. The effectiveness of two such techniques was investigated and the results reported in this project.

This development intends to provide a cost efficient solution for applications involving on-board Processing of RF signals or Data Collection, for low bandwidth missions, targeting in particuliar Internet-of-Things (IoT) / low data rate Machine-To-Machine (M2M) communications, but also spectrum survey, geo-location, data collection in general.

In this project, the Space Norway led consortium with Kongsberg Seatex and FFI have
measured the actual downlink performance of the world´s first VHF Data Exchange System (VDES) payload in space under realistic conditions in the Arctic and at other locations. At the time of contract award, in 2015, the downlink waveforms were not specified and no satellite capacity was available.

ESA ARTES C&G program supports MDA in the development and qualification of new antenna design in a context of a megaconstellation. Manufacturing, assembly and testing methods suitable for larger volume production of spacecraft antenna will be demonstrated in order to meet the demand of current and future satellite constellations.

THALES ALENIA SPACE IN FRANCE is looking for solutions to improve
its competitiveness in terms of Ka-band equipments, payloads and
satellites. As far as Ka-band output filtering is concerned, use of
Temperature Compensated OMUX is foreseen. This technology leads to
an improvement of the input power limitation, footprint, useful bandwidth
and electrical in band performances
The five channels high power Ka band full TC OMUX qualification allows
to increase the competitiveness of THALES ALENIA SPACE IN FRANCE
products by fulfilling identified customer requirements as Military, DTH
analogic, HTS and VHTS satellite applications.

The SCNE enables to study and assess protocol performances of new LEO constellations, ranging from low speed data collection and mobile communications, to broadband and broadcast services.
The co-simulation approach, which couples orbital and network simulation, facilitates the correlation between network and orbital events and enables to analyze long simulation periods in a short time frame.

The Rx2 unit is the second-generation command receiver designed and manufactured at Kongsberg Norspace. The command receiver is to be used for spacecraft telemetry, tracking and commands (TT&C). The Unit design is in-orbit programmable up to 750MHz bandwidth, and prepared for receiving commands and ranging signals at C-band, Ku-band or Ka-band.

RUAG Space AB have developed and qualified horn assemblies for global Ku-Band coverage TTC, Ka-Band IOT payload Rx/Tx and Beacon. The RUAG GNSS antenna design has within the scope of work evolved to withstand harsher random environment. All antennas are well adapted for new platforms such as NEOSAT.

This project represents the basis for enabling satellite systems using beam hopping capabilities. Beam hopping, based on the DVB-S2X transmission standard, enables time sharing of satellite capacity among different beams, making satellite systems more flexible and efficient. The satellite performs demultiplexing of the uplink signal and distribution via periodic switching of the satellite beam to different coverage areas. The switching time plan as well as the addressed coverage areas and coverage shapes can be reconfigured according to actual needs.
In the context of such activity, a modulator, two terminals, as well as a beam-switching payload emulator are developed using the DVB-S2X Super-Framing Format 4 waveform.

LOCOMO project is envisaged to design and develop a low cost and compact Ka-band mobile satcom terminal, which provides broadband on-the-move communications to emergency, governmental and security networks.

Airbus Defence and Space Netherlands (ADSN) has developed, and continuously updated over the past two decades, a non-explosive low shock Hold Down and Release System for its Advanced Rigid Array and Flatpack Solar Array families. Many hundreds of these systems have released a variety of solar arrays and other deployable systems with 100% success. The NELS program objective is to develop a substitute for the existing Hold Down and Release System, which is more robust and has an extended preload capacity.

The objective of this proposal was to design and develop the next generation of Mission Control Centre (MCC NG), to propose a complete and optimised solution to operate simply and maximize the capacity of future flexible payloads.