| ARTEM - Aircraft Noise Reduction Technologies and related Environmental IMpact | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/artem/ARTEM - Aircraft Noise Reduction Technologies and related Environmental IMpact | ARTEM - Aircraft Noise Reduction Technologies and related Environmental IMpact | The main objective of ARTEM is to define novel aircraft configurations for 2035 (tube/wing) and 2050 (Blended Wing Body with conventional UHBR propulsion system and with distributed electrical propulsion). |
| CASTLE - CAbin Systems design Toward passenger welLbEing | | https://www.cira.it/en/aeronautics/safety-e-security-air-transport/castle/CASTLE - CAbin Systems design Toward passenger welLbEing | CASTLE - CAbin Systems design Toward passenger welLbEing | CASTLE objective is to develop, design and test with a Technology Readiness Level (TRL) 5 a new aircraft cabin for both Regional Aircraft and Business Jet, with the aim of increasing passenger’s well-being. |
| COAST - COst-effective Avionic SysTem | | https://www.cira.it/en/aeronautics/safety-e-security-air-transport/coast/COAST - COst-effective Avionic SysTem | COAST - COst-effective Avionic SysTem | The project aims to develop a low cost avionic system to be implemented on the SAT aircraft (Small Air Transport), designed to passengers transport (up to 19 passengers), in order to enable the single-pilot operations. |
| DANTE - Development of Aero-vibro-acoustics Numerical and Technical Expertise | | https://www.cira.it/en/aeronautics/safety-e-security-air-transport/dante/DANTE - Development of Aero-vibro-acoustics Numerical and Technical Expertise | DANTE - Development of Aero-vibro-acoustics Numerical and Technical Expertise | This project aims to strengthen and expand the skills and capabilities in computational aero-vibro-acoustic. DANTE objective is, on one side, to increase the competitiveness of CIRA and, on the other side, to extend the use of current aero-vibroacoustic tools in industrially relevant applications. |
| EATS - Efficient Air Transport System | | https://www.cira.it/en/aeronautics/safety-e-security-air-transport/eats/EATS - Efficient Air Transport System | EATS - Efficient Air Transport System | |
| 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. |
| GRADE - GNSS Solutions for Increased GA and Rotorcraft Airport Accessibility Demonstration | | https://www.cira.it/en/aeronautics/sistemi-di-bordo-e-atm/grade/GRADE - GNSS Solutions for Increased GA and Rotorcraft Airport Accessibility Demonstration | GRADE - GNSS Solutions for Increased GA and Rotorcraft Airport Accessibility Demonstration | The project aims to demonstrate, through in-flight trials, the ability of General Aviation aircraft and rotorcraft to take advantage of the concepts developed in the SESAR1 program, in order to facilitate the integration of these aircraft into airspace and airports where the SESAR concepts are implemented. |
| INVIRCAT - Investigate IFR RPAS Control in Airports and TMA | | https://www.cira.it/en/aeronautics/sistemi-di-bordo-e-atm/invircat/INVIRCAT - Investigate IFR RPAS Control in Airports and TMA | INVIRCAT - Investigate IFR RPAS Control in Airports and TMA | The INVIRCAT project investigates innovative solutions for a safe, equal and efficient integration of RPAS into the existing Air Traffic Control ( ATC ) procedures and infrastructures |
| 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. |
| 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. |
| 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. |
| 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. |
| VENUS - inVestigation of distributEd propulsion Noise and its mitigation through wind tUnnel experiments and numerical Simulations | | https://www.cira.it/en/aeronautics/fixed-wing-air-vehicle/venus/VENUS - inVestigation of distributEd propulsion Noise and its mitigation through wind tUnnel experiments and numerical Simulations | VENUS - inVestigation of distributEd propulsion Noise and its mitigation through wind tUnnel experiments and numerical Simulations | The European research project VENUS aims at improving the knowledge about the aerodynamic and aeroacoustic performance of a wide range of DEP configurations through numerical simulations and wind tunnel test experiments. |
