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. |
FLPP3-DOC Demise Observation Capsule | | https://www.cira.it/en/space/sistemi-di-bordo-per-le-piattaforme-spaziali/flpp3-doc/FLPP3-DOC Demise Observation Capsule | FLPP3-DOC Demise Observation Capsule | DOC is an European Project aimed to the design and integration of a first black box prototype for the acquisition of data on the demise of the upper stages of space launch vehicles. |
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. |
LIPROM – Liquid Propulsion Research on Oxygen Methane | | https://www.cira.it/en/space/space-propellers/liprom/LIPROM – Liquid Propulsion Research on Oxygen Methane | LIPROM – Liquid Propulsion Research on Oxygen Methane | A co-operation between ASI and JAXA has been promoted in order to investigate, by means of a research and development program, the characteristics of liquid methane for space propulsion applications. |
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. |
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. |
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. |
USV - Unmanned Space Vehicle | | https://www.cira.it/en/competences/aerothermodinamics/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. |