SMARTEES
MULTIFUNCTIONAL COMPONENTS FOR AGRESSIVE ENVIROMENTS IN SPACE APPLICATIONS
| Coordinatore | FUNDACION TECNALIA RESEARCH & INNOVATION
Organization address
address: PARQUE TECNOLOGICO DE MIRAMON PASEO MIKELETEGI 2 contact info |
| Nazionalità Coordinatore | Spain [ES] |
| Sito del progetto | http://www.smartees-project.eu/ |
| Totale costo | 2˙688˙900 € |
| EC contributo | 1˙971˙938 € |
| Programma | FP7-SPACE
Specific Programme "Cooperation": Space |
| Code Call | FP7-SPACE-2010-1 |
| Funding Scheme | CP |
| Anno di inizio | 2011 |
| Periodo (anno-mese-giorno) | 2011-01-01 - 2013-12-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
FUNDACION TECNALIA RESEARCH & INNOVATION
Organization address
address: PARQUE TECNOLOGICO DE MIRAMON PASEO MIKELETEGI 2 contact info |
ES (DONOSTIA-SAN SEBASTIAN) | coordinator | 568˙251.70 |
| 2 |
POLITECNICO DI TORINO
Organization address
address: Corso Duca degli Abruzzi 24 contact info |
IT (TORINO) | participant | 343˙499.60 |
| 3 |
"NATIONAL CENTER FOR SCIENTIFIC RESEARCH ""DEMOKRITOS"""
Organization address
address: Patriarchou Gregoriou Str. contact info |
EL (AGHIA PARASKEVI) | participant | 247˙749.50 |
| 4 |
Erbicol SA
Organization address
address: Viale Pereda 22 contact info |
CH (Balerna) | participant | 239˙339.50 |
| 5 |
AIRBUS DEFENCE AND SPACE GMBH
Organization address
address: WILLY MESSERSCHMITT STRASSE 1 contact info |
DE (OTTOBRUNN) | participant | 214˙762.50 |
| 6 |
SCUOLA UNIVERSITARIA PROFESSIONALE DELLA SVIZZERA ITALIANA (SUPSI)
Organization address
address: STABILE LE GERRE contact info |
CH (MANNO) | participant | 201˙585.20 |
| 7 |
Aerospace & Advanced Composites GmbH
Organization address
address: Viktor-Kaplan-Strasse 2 contact info |
AT (Wiener Neustadt) | participant | 156˙750.00 |
Mappa
Word cloud
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
Obiettivo del progetto (Objective)
'The aim of this proposal is the development of ceramic composites structures which are needed for applications in aggressive environments, where (oxidative) and temperatures are required, such as hot parts of space vehicles for orbital re-entry (reusable launcher vehicles, RLVs). The solution will be focused on re-usable systems.
As expressed by the European Commission a non-dependent access to the critical space technology is required at European level. Therefore the strategy is to focus on materials systems able to be in a medium term independent from the technologies that already exist outside Europe (mainly in USA, China and Russia).
The technical approach is focused on the development of multilayer concept based on high temperature ceramics (HTCs) and ultrahigh temperature ceramics (UHTCs) with multiple tailored properties. Their joining processes to conventional structural ceramic matrix composites (CMCs) or novel porous sandwich structures, and the final attachment to metallic structures.
The MULTIFUNCTIONAL COMPONENT can be broken down at three levels:
• 1st Level: This will be composed of multilayers. • 2nd Level: This will be composed of qualified CMCs or novel CMC-SiC foam sandwich structures. • 3thLevel: This will be composed of the metallic structural frames.
A TPS technology sample design will be provided and will be aided by material's modelling and simulation via conventional methods and computed tomography will be used to obtain a real FEM model. The output will be to determine critical parameters such as thicknesses and geometries.
The technology sample will be ground tested for simulation of the re-entry conditions and will determine the fundamental performance and the degradation mechanisms. The results will be reviewed in comparison with the outputs of TPS requirements and environment specifications. This will result in the completion of the validation of the TPS performance and the assessment of achievement of a TRL 4-5.'
Introduzione (Teaser)
Re-entry of space vehicles subjects them to extreme temperatures and aggressive conditions promoting oxidation. Novel multi-layered protection based on advanced ceramics and foam could be the basis of the first EU-sourced space-critical heat shield.