|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.|
| 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. |
|SOLverATD - An efficient solver for Aerothermodynamics||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/solveratd/SOLverATD - An efficient solver for Aerothermodynamics||SOLverATD - An efficient solver for Aerothermodynamics||The main goal of the project is the development of a numerical solver for aerothermodynamic applications with the aim to consolidate the key role of CIRA in the field of numerical simulation of reacting flows in the European scenario.|
|SOLRAM - Solid Rocket Motors ||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/solram/SOLRAM - Solid Rocket Motors||SOLRAM - Solid Rocket Motors ||The goal of SOLRAM Project is to develop at CIRA competences in the field of solid rocket motors, with special regard to the evaluation of heat fluxes on the internal walls of the chamber and to the phenomenon of pressure oscillations inside the chamber itself. |
|ABLAMOD - Advanced aBLAtion characterization and MODelling||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/ablamod/ABLAMOD - Advanced aBLAtion characterization and MODelling||ABLAMOD - Advanced aBLAtion characterization and MODelling||The ABLAMOD project aims to make a substantial progress for the design of an ablative thermal protection system by incorporating aspects of high fidelity mesoscale ablator physics within a modular framework. |
|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.
|ISAA – Imaging antenna System based on Aperiodic feeding Arrays||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/isaa/ISAA – Imaging antenna System based on Aperiodic feeding Arrays||ISAA – Imaging antenna System based on Aperiodic feeding Arrays||The ISAA project intends to develop an innovative imaging antenna system.|
|MEFIA – Novel Physics Methodologies for Aerospace||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/mefia/MEFIA – Novel Physics Methodologies for Aerospace||MEFIA – Novel Physics Methodologies for Aerospace||The purpose of the activity is to develop an innovative technique which allows simultaneously to obtain information both on the wearing of materials and on the temperature at which the wearing takes place, to achieve the use of the techniques in-flight. |
|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.|
|OPPLA Process Parameters Optimization for the EBM system||https://www.cira.it/en/space/accesso-allo-spazio-satelliti-ed-esplorazione/oppla/OPPLA Process Parameters Optimization for the EBM system||OPPLA Process Parameters Optimization for the EBM system||In the OPPLA project it is proposed to investigate on the EBM process parameters in order to identify those ones that mainly influence the morphological and mechianical properties of the components manufactured by EBM Tech.|
|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.|
|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. |