309 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 309 total) Characterization of W-band propagation channel through ground-based observations The use of higher frequencies is becoming necessary for supporting feeder links of High Throughput Telecom Satellites due to the larger bandwidths available. Q and V bands are now being considered as a baseline for next generation systems. The next step will be to look at W band. In order to understand the system sizing, it is necessary to have a good modelling of the propagation channel. So far no measurement campaign has been done, therefore it is needed to start characterizing the channel. Italy TDE T507-411EE Sapienza University of Rome 2018 - 2023 Characterization of W-band propagation channel through ground-based observations An Ultracompact Hyperspectral imager in the Thermal Infrared The activity followed the development of an innovative hyperspectral imaging system for remote sensing applications in the thermal infrared. The camera is compact, lightweight and robust. The activity covered the development of the three modules of the imager, namely the spectrometer, the telescope and the detector. The consortium designed and manufactured an innovative spectrometer based on Fourier transform spectroscopy, consisting on calomel birefringent crystals, with working range in the thermal infrared. Italy Discovery S 2021-11 CNR 2022 - 2023 An Ultracompact Hyperspectral imager in the Thermal Infrared Innovative scalable large deployable antenna reflectors Despite different attempts performed in the past two decades, Europe is lacking a competitive product for a large reflector with the requested TRL level to embark on a commercial program. Need is identified to cover antenna applications from 4 up to 18 meter and for frequencies from UHF up to Ka band.. American companies are leaders in this domain and are commercially dominating the worldwide market. Italy TDE T515-301MS THALES ALENIA SPACE ITALIA SPA 2012 - 2023 Innovative scalable large deployable antenna reflectors De-risk assessment: Feasibility assessment on the reuse of a deep-space Nanosatellite platform for a fast planetary defence mission . Italy GSTP G617-241TAju Tyvak International srl 2023 - 2023 De-risk assessment: Feasibility assessment on the reuse of a deep-space Nanosatellite platform for a fast planetary defence mission Dark optical nano-spectroscopy in the visible and near-IR spectrum Diffraction limits the resolution of standard optical microscopes. Breaking the diffraction limit is the motivation behind Scanning Probe Microscopy (SPM) that includes Atomic Force Microscopy (AFM) and Near-field Scanning Optical Microscopy (SNOM). SPMs create high-resolution maps of the sample’s surface by scanning the sample with nanometric probes. SNOM in particular, can simultaneously provide information on the morphology and on the optical properties of materials by illuminating the sample with a localized field provided by the microscope probe. Italy Discovery EISI_I-2021-00501 Istituto Italiano di Tecnologia 2021 - 2023 Dark optical nano-spectroscopy in the visible and near-IR spectrum Novel Lunar Surface Power Plant - European Charging Station pre-phase A The European Charging Station for the Moon (ECSM) is to be integrated within the EL3 Architecture, which provides the function of transportation of ECSM to the lunar surface. The Power Station mission is envisaged as possible EL3 payload and it aims at providing power, at a strategic location on the lunar surface, during lunar day and night to ESA and International partner assets. It is in line with the envisioned international lunar exploration architecture. Italy Preparation 21-P-M-HRE-04-b Thales Alenia Space Italia S.p.A 2022 - 2023 Novel Lunar Surface Power Plant - European Charging Station pre-phase A Exploiting numerical modelling for the characterisation of collision break-ups All missions in Earth-bound orbits rely on space debris and meteoroid flux models. These models are used to assess the mission risk and design shielding concepts (for manned modules). The flux predictions have been found to have a remarkable sizing effect. Collision break-ups are the major source of debris >1mm and are poorly understood. This needs to be improved significantly. On Agency level, collision break-up modelling is decisive to define the Agency's position towards international agreements on space debris mitigation. Current models will be misleading. Italy TDE T711-603SD SPACEDYS S.R.L. SPACE DYNAMICS SERVICES S.R.L. 2020 - 2023 Exploiting numerical modelling for the characterisation of collision break-ups 120 W 32 GHz TWT for Payload Data Transmitter New scientific missions require Ka-Band high power sources for the data return. Limitation on maximum antenna size and minimum required data rate can be overcome by increasing the transmitted power. At present, there is no off the shelf TWT(A) in the allocated frequency band (31800-32300 MHz) in Europe with 120W saturated output power. Instead, a 250W TWT in the range 17700 - 20200 MHz is under qualification and the feasibility of 100W TWT in the range 37500 - 42500 MHz has been recently demonstrated by test in a breadboard. Italy TDE T206-015ES Leonardo S.p.a. 2020 - 2023 120 W 32 GHz TWT for Payload Data Transmitter Innovative Propulsion Systems for cubesats and microsats With the underway exploitation of cubesats and microsats for commercial, Science and Earth Observation missions and the ongoing development of super-constellations of Micro/minisats, it has become obvious the need to develop European, reliable, affordable and yet performing Propulsion Systems serving these class of satellites. The introduction of propulsion functions on these classes of satellites is dramatically enhancing their performances and utilisation perspectives. Italy TDE T719-602MP UNIVERSITA DI PISA 2020 - 2023 Innovative Propulsion Systems for cubesats and microsats Modular Scanning Array based on Simple Antenna Manufacturing The main goal of MOSAIC project consists in the design of an AESA improving the technical and commercial maturity of the antenna architectures proposed in the ESA invention [1] which describes a design and manufacturing method for large sparse phased arrays for geostationary Earth orbit (GEO) satellite. Sparse arrays offer power consumption reduction through a not regular lattice, at the cost of increasing the complexity of the beam forming network (BFN) as well as a not complete filling of the available aperture. 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