|C.A.DI.R.A CapsulA DI Rientro Atmosferico||https://webauthoring.cira.it/en/research/Pages/C-A-DI-R-A-CapsulA-DI-Rientro-Atmosferico.aspx||C.A.DI.R.A CapsulA DI Rientro Atmosferico||The CADI.RA project aimes at the design, development, validation and certification of a re-entry capsule demonstrator for future applications such as re-entry from the International Space Station, microgravity experiments and landings on other planets .|
|ABLAMOD - Advanced aBLAtion characterization and MODelling||https://webauthoring.cira.it/en/research/Pages/ABLAMOD---.aspx||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://webauthoring.cira.it/en/research/Pages/HEXAFLY-INT.aspx||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://webauthoring.cira.it/en/research/Pages/INTERSTADIO-GRID.aspx||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.
|MEFIA – Novel Physics Methodologies for Aerospace||https://webauthoring.cira.it/en/research/Pages/MEFIA.aspx||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://webauthoring.cira.it/en/research/Pages/METMAT.aspx||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://webauthoring.cira.it/en/research/Pages/MINI-IRENE.aspx||Mini-IRENE FLIGHT EXPERIMENT||Mini-IRENE is a technology demonstrator of advanced thermal protection systems for the atmospheric re-entry.|
| Space Rider PRIDE||https://webauthoring.cira.it/en/research/Pages/PRIDE.aspx|| 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. |
|TB-GRID - A Satellite central tube and a boom for deployable antennas to be manufactured in composite materials ||https://webauthoring.cira.it/en/research/Pages/TB-GRID.aspx||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.|
|ATDTEC - TEChnologies for AeroThermoDynamics||https://webauthoring.cira.it/en/research/Pages/ATDTEC.aspx||ATDTEC - TEChnologies for AeroThermoDynamics||Aerothermodynamics is an essential discipline for the design of hypersonic aircrafts, capsules or space shuttles for re-entry into the Earth's atmosphere, as well as capsules for interplanetary missions|
|VECEP - Studies on aerothermodynamics, acoustic and vibroacoustic of the VEGA C takeoff||https://webauthoring.cira.it/en/research/Pages/VECEP.aspx||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. |