| Space Rider PRIDE | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/pride/Space Rider PRIDE | Space Rider PRIDE | Space-Rider is an European Space Agency Program devoted to the development of a reusable space transportation system capable of performing in-orbit operations as payload capturing from the International Space Station and Microgravity experimentation and then to land on a runway. |
| AIRGREEN 2 - Morphing Wing Technology | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/air-green-2/AIRGREEN 2 - Morphing Wing Technology | AIRGREEN 2 - Morphing Wing Technology | Development of technologies for in-flight wing adaptation to improve aerodynamic efficiency of new generation regional aircrafts. |
| AMICO - Additive Manufacturing and automatic process for hybrid and composite materials | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/amico/AMICO - Additive Manufacturing and automatic process for hybrid and composite materials | AMICO - Additive Manufacturing and automatic process for hybrid and composite materials | The Amico project is aimed at using of additive processes, namely to generate the component slice after slice and then to compose it into a 3D geometry using not necessarily powders or metal filaments, but carbon fibers and resins thermoplastic or thermosetting and realizing hybrid systems... |
| DEFENDER - DEsign, development, manufacture, testing and Flight qualification of nExtgeNeration fuel storage system with aDvanced intEgRated gauging and self-sealing capabilities | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/defender/DEFENDER - DEsign, development, manufacture, testing and Flight qualification of nExtgeNeration fuel storage system with aDvanced intEgRated gauging and self-sealing capabilities | DEFENDER - DEsign, development, manufacture, testing and Flight qualification of nExtgeNeration fuel storage system with aDvanced intEgRated gauging and self-sealing capabilities | The DEFENDER project aims at the design, manufacturing and testing of the fuel storage system for the NGCTR-TD (Next Generation Civil TiltRotor - Technology Demonstrator) up to TRL6 |
| FTB4UAS Flight Test Bed For UAS | | https://www.cira.it/en/aeronautics/aeromobili-pilotati-da-remoto-e-non-pilotati/ftb4uas/FTB4UAS Flight Test Bed For UAS | FTB4UAS Flight Test Bed For UAS | Development of flight testing demonstrators for the flight validation of enabling technologies in the field of autonomous flight technologies, innovative aerostructures and hybrid propulsion systems. |
| HEXAFLY-INT - High-Speed Experimental Fly Vehicles-International | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/hexafly-int/HEXAFLY-INT - High-Speed Experimental Fly Vehicles-International | HEXAFLY-INT - High-Speed Experimental Fly Vehicles-International | The HEXAFLY-INT, High-Speed Experimental Fly Vehicles – International, project, stemmed from the interest of Europe in hypersonic civil transportation vehicles, is dedicated to the development of a flight test experiment for demonstrating and validating high speed key technologies. |
| INTERSTADIO GRID - The Interstage 2/3 of the new European launcher, VEGA C | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/interstadio-grid/INTERSTADIO GRID - The Interstage 2/3 of the new European launcher, VEGA C | INTERSTADIO GRID - The Interstage 2/3 of the new European launcher, VEGA C | CIRA in partnership with Avio is involved in the development and qualification of the interstage 2/3 of the new European launcher, VEGA C, in the frame of the VECEP Program of ESA.
The new Interstage will be constituted by a composite grid structure, characterized by a low weight and high structural properties.
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| LED - Long Endurance Demonstrator | | https://www.cira.it/en/aeronautics/aeronautical-propellers/led/LED - Long Endurance Demonstrator | LED - Long Endurance Demonstrator | This project aims at the realization of a primary and secondary power system based on electrochemical modules, suitable for aerospace applications. |
| METMAT - Development of Microstructured Materials | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/metmat/METMAT - Development of Microstructured Materials | METMAT - Development of Microstructured Materials | The project Microstructured materials/Metamaterials aims at developing the theoretical and numerical tools for the modelling of the mechanical properties of materials with a defined, architecture microstructure. |
| Mini-IRENE FLIGHT EXPERIMENT | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/mini-irene/Mini-IRENE FLIGHT EXPERIMENT | Mini-IRENE FLIGHT EXPERIMENT | Mini-IRENE is a technology demonstrator of advanced thermal protection systems for the atmospheric re-entry. |
| SAT-AM More Affordable Small Aircraft Manufacturing | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/sat-am/SAT-AM More Affordable Small Aircraft Manufacturing | SAT-AM More Affordable Small Aircraft Manufacturing | The aim of SAT-AM project is to develop low cost manufacturing technologies able to assure weight saving and equal levels of safety and reliability for General Aviation class vehicle. |
| SMAF – Smart AirFrame | | https://www.cira.it/en/aeronautics/aeromobili-pilotati-da-remoto-e-non-pilotati/smaf-–-smart-airframe/SMAF – Smart AirFrame | SMAF – Smart AirFrame | Development of an innovative design criteria for the reduction of the weight and cost of the primary structures made of composite material, also by means of out-of-autoclave process, through the use of information coming from structural health monitoring systems (SHM). |
| SMOS – SMART ON-BOARD SYSTEMS | | https://www.cira.it/en/aeronautics/aeromobili-pilotati-da-remoto-e-non-pilotati/smos-–-smart-on-board-systems/SMOS – SMART ON-BOARD SYSTEMS | SMOS – SMART ON-BOARD SYSTEMS | The project SMOS (SMart On-board Systems) aims to develop technologies concerning on-board systems such as low weight and low power Anti-Icing / De-Icing devices as well as diagnostic and prognostic systems. The SMOS project is funded by PRO.R.A. |
| T-WING - Tilt Rotor Wing | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/t-wing/T-WING - Tilt Rotor Wing | T-WING - Tilt Rotor Wing | T-WING consortium is working on the composite wing of the Next Generation Civil TiltRotor - Technology Demonstrator, planned to be flying in 2023. The task undertaken by the consortium is aimed at designing, manufacturing, qualifying and flight-testing the wing and moveable surfaces of the NGCTR-TD. |
| TB-GRID - A Satellite central tube and a boom for deployable antennas to be manufactured in composite materials | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/tb-grid/TB-GRID - A Satellite central tube and a boom for deployable antennas to be manufactured in composite materials | TB-GRID - A Satellite central tube and a boom for deployable antennas to be manufactured in composite materials | TB Grid Project aims to design and manufacture by means of automated processes a satellite central tube and a boom for deployable antennas to be manufactured in composite materials with a grid architecture. |
| TEAM - Maturation of Innovative Technologies for ALM | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/team/TEAM - Maturation of Innovative Technologies for ALM | TEAM - Maturation of Innovative Technologies for ALM | Additive manufacturing, also known with the acronym ALM (Additive Layer Manufacturing), is a production method that, using very different technologies, allows the creation of 3D objects (parts, components, semi-finished or finished products) by adding material. |
| TIMA – Technologies for low emission and long endurance piston engines | | https://www.cira.it/en/aeronautics/aeronautical-propellers/tima/TIMA – Technologies for low emission and long endurance piston engines | TIMA – Technologies for low emission and long endurance piston engines | The project aims at the definition, development and application of enabling technologies for the development of piston engines, for General Aviation aircraft (GA) and for Unmanned Aerial Vehicle (UAV) applications, with low environmental impact and high autonomy. |
| USV - Unmanned Space Vehicle | | https://www.cira.it/en/competences/strutture-e-materiali/USV - Unmanned Space Vehicle | USV - Unmanned Space Vehicle | Il programma Unmanned Space Vehicle sviluppa sistemi e tecnologie per un accesso allo spazio indipendente, affidabile ed efficace con l’obiettivo di sviluppare tecnologie per il trasporto ipersonico ... |
| VECEP - Studies on aerothermodynamics, acoustic and vibroacoustic of the VEGA C takeoff | | https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/vecep/VECEP - Studies on aerothermodynamics, acoustic and vibroacoustic of the VEGA C takeoff | VECEP - Studies on aerothermodynamics, acoustic and vibroacoustic of the VEGA C takeoff | Lo sviluppo del nuovo lanciatore VEGA C migliorerà la capacità di carico di circa il 50% rispetto alla configurazione attuale di VEGA ed avrà anche una maggior flessibilità operativa. |
