137 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 137 total) De-risk assessment: Graphene-based materials with improved gas barrier properties for space applications The aim of the activity, developed by Omnidea-RTG in conjunction with ESA, Pleione SA and Fraunhofer IVV, was to produce a thin film polymer-based product enhanced with Graphene nanoparticles to decrease He gas permeability while maintaining thermal bonding properties and without major penalties in UV resistance, for use in high-altitude inflatable structures. The proposed technological application is the usage of this thin film as envelope inner layer for high altitude airborne platforms which, from a lower altitude (vs. Germany GSTP G617-241TAbg OMNIDEA-RTG GMBH 2018 - 2021 De-risk assessment: Graphene-based materials with improved gas barrier properties for space applications UniverSAS Power Supply Extension A Power SCOE tests and simulates the power subsystems of a spacecraft e.g. ;solar arrays, battery, umbilical connection, electronic load (e.g payload load) and other related functions. It comprises power supplies and loads and control functions. Austria GSTP GT27-014EP ATOS CONVERGENCE CREATORS GMBH 2018 - 2021 UniverSAS Power Supply Extension MicroMHiDe: Technologies for Microsatellites Multispectral High Definition Imager. The development of miniaturized high performance avionics allows the building of microsatellites platforms with the high pointing stability and accuracy. This new generation of microsatellites could embark high-resolution optical systems, but given limited volume and power, the instrument will be limited in SNR. A new generation of hybrid detectors, known as CCD-in-CMOS detectors, can allow circumventing SNR limitations by operating in Time Delay Integration (TDI). This type of operation was, until recently, limited to CCD detectors that are very costly and power hungry. Belgium GSTP GT11-016MM Aerospacelab 2018 - 2021 MicroMHiDe: Technologies for Microsatellites Multispectral High Definition Imager. Space Rated Microcontroller Softcore - Product development. In the current space market the increasing systems complexity poses great challenges to architects, designers and verification engineers. Systems requirements are continuously asking more functionality with less power, less resources, less time and cost, forcing suppliers to shrink their schedules. One important aspect that is becoming more and more critical nowadays is a 'first time right' design that can be scalable and adaptable to special needs, leveraging on the reuse of building blocks which are highly configurable and already validated. Slovenia GSTP GT17-121ED SKYLABS D.O.O. 2018 - 2021 Space Rated Microcontroller Softcore - Product development. VDES pre-operational demonstration for navigation augmentation and VHF maritime spectrum monitoring The pre-operation demonstration will be used as a proof of concept towards the World-Radio Conference to demonstrate the feasibility of the VDES in a representative in the field trail. The activity will also provide the capability of monitoring the VHF maritime spectrum both from external interference sources (such as land mobile) as well as intra-system interference caused by VDES different components (such as VDE terrestrial components). Norway GSTP GT17-113ES SPACE NORWAY AS 2018 - 2021 VDES pre-operational demonstration for navigation augmentation and VHF maritime spectrum monitoring De-risk assessment: Liquid Oxygen Turbopump The majority of large engine activity in Europe is hydrogen based and requires more costly pump technology, with deep cryogenic temperatures and complex sealing requirements. This activity was to demonstrate a low-cost LOX pump design, manufacture and test capability with view to enabling a LOX Kerosene 60kN engine program. These engines are more appropriate for the small launcher market than LOX/LH2. United Kingdom GSTP G617-241TAad LENA Space 2018 - 2021 De-risk assessment: Liquid Oxygen Turbopump Utilisation of a Heavy and Light Ion Facility at UCL for Component Radiation Studies This activity concerns execution of regular irradiation test campaigns on EEE components for flight on ESA and European space missions. Up to 360 hours per year of beam time is available free of charge on a priority basis for ESA. Additionally, a minimum of 500 hours per year is available for ESA sub-contractors, research institutes and other interested users at preferential hourly rates. The agency provides the facility with a detailed work programme of the test campaigns. Subsequently, the facility performs test campaign scheduling (in agreement with the Agency). Belgium TDE T723-F09QE Universite catholique de Louvain 2018 - 2021 Utilisation of a Heavy and Light Ion Facility at UCL for Component Radiation Studies Atmospheric Missions DAta packaging (AMIDA) The core of the activity is the development and demonstration of technologies to homogenize the data for joint use: this is highly relevant for Atmospheric Sciences data where a large variety of data in terms of sensing time and geometry and dimensionality (1D to 3D) prevent the combined use of various datasets. Nevertheless, the developed methodologies can be applied to other domains, to create meaningful subsets to cope with the growing of the data stream (large amount of EO data coming from different platforms for the same domain). Austria GSTP G611-049EO SISTEMA GMBH 2018 - 2021 Atmospheric Missions DAta packaging (AMIDA) Environmentally friendly corrosion protective hybrid coating as substitute of chromium based conversion coatings for space applications IRUCOAT is an eco-friendly hybrid sol-gel coating based on SiO2-Zr02-organic epoxy interconnected network, developed by TECNALIA and already tested for corrosion protection and other performance requirements applicable to the aerospace sector. Spain TDE B02017085 FUNDACION TECNALIA RESEARCH & INNOVATION 2018 - 2021 Environmentally friendly corrosion protective hybrid coating as substitute of chromium based conversion coatings for space applications Flexible and reconfigurable TT C Transponder with Payload Data Transmission Satellites in all application domains include a communication subsystem with similar core functions, specific features, and different operating frequencies. ;;Central to this subsystem is the Transponder equipment. ;Its current implementations already include flexibility in terms, e.g. of modulation and coding schemes. ;However missions placing specific requirements must still bear the cost of adaptations. ;Moreover the accommodation (power, mass) of such equipment is a burden for smaller missions. 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