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 |
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. |
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. |
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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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. |
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). |
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. |
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/research-infrastructures/advanced-materials-and-processes/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. |