ATLLAS II
Aero-Thermodynamic Loads on Lightweight Advanced Structures II
| Coordinatore | EUROPEAN SPACE AGENCY
Organization address
address: Rue Mario Nikis 8-10 contact info |
| Nazionalità Coordinatore | France [FR] |
| Totale costo | 6˙536˙057 € |
| EC contributo | 4˙750˙000 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2011 |
| Periodo (anno-mese-giorno) | 2011-05-01 - 2015-10-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
EUROPEAN SPACE AGENCY
Organization address
address: Rue Mario Nikis 8-10 contact info |
FR (PARIS) | coordinator | 535˙677.79 |
| 2 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | participant | 1˙432˙509.76 |
| 3 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | participant | 792˙119.00 |
| 4 |
TOTALFORSVARETS FORSKNINGSINSTITUT
Organization address
address: Gullfossgatan 6 contact info |
SE (STOCKHOLM) | participant | 367˙701.75 |
| 5 |
MBDA FRANCE SAS
Organization address
address: BOULEVARD DE MONTMORENCY 37 contact info |
FR (PARIS) | participant | 324˙923.00 |
| 6 |
GAS DYNAMICS LTD
Organization address
address: 22 Empress Avenue contact info |
UK (FARNBOROUGH) | participant | 199˙723.20 |
| 7 |
UNIVERSITAET STUTTGART
Organization address
address: Keplerstrasse 7 contact info |
DE (STUTTGART) | participant | 196˙270.80 |
| 8 |
INSTITUTUL NATIONAL DE CERCETARI AEROSPATIALE ELIE CARAFOLI - I.N.C.A.S. SA
Organization address
address: IULIU MANIU 220 SECTOR 6 contact info |
RO (BUCURESTI) | participant | 181˙830.00 |
| 9 |
TISICS Limited
Organization address
address: Invincible Road 22 contact info |
UK (Farnborough) | participant | 181˙830.00 |
| 10 |
SITAEL SPA
Organization address
address: VIA S SABINO 21 contact info |
IT (MOLA DI BARI) | participant | 167˙509.50 |
| 11 |
AIRBUS DEFENCE AND SPACE GMBH
Organization address
address: WILLY MESSERSCHMITT STRASSE 1 contact info |
DE (OTTOBRUNN) | participant | 146˙017.00 |
| 12 |
UNIVERSITY OF SOUTHAMPTON
Organization address
address: Highfield contact info |
UK (SOUTHAMPTON) | participant | 146˙017.00 |
| 13 |
UNIVERSITE PIERRE ET MARIE CURIE - PARIS 6
Organization address
address: Place Jussieu 4 contact info |
FR (PARIS) | participant | 77˙871.20 |
| 14 |
Nome Ente NON disponibile
Organization address
address: BRYGGERIVAGEN 9 contact info |
SE (BROMMA) | participant | 0.00 |
| 15 |
ALTA SPA
Organization address
address: Via Allessandro Gherardesca 5 contact info |
IT (PISA) | participant | 0.00 |
Mappa
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Obiettivo del progetto (Objective)
'ATLLAS II is a logical follow-up of a recently finalized FP6 project which has as objectives the identification and assessment of advanced light-weight and high-temperature resistant materials for high-speed vehicles up to Mach 6.
The material requirements are first defined through an in-depth feasibility study of a Mach 5-6 vehicle. The consortium has now this capability at hand as they can rely on a first set of validated tools, material databases and valuable experience acquired during ATLLAS-I. Starting with a preliminary aero-thermal-structural high-speed vehicle design process, further multi-disciplinary optimization and testing will follow to result into a detailed layout of an independently European defined and assessed high-speed vehicle. Special attention will be given to alleviate sonic boom and emissions at high altitudes.
Throughout the design process, the aero-thermal loads will define the requirements for the proposed materials and cooling techniques needed for both the airframe and propulsion components. The former will focus on sharp leading edges, intakes and skin materials each coping with different external aero-thermal loads. The latter will be exposed to internal combustion driven loads. Both metallic (Titanium Matrix Composites and Ni-based Hollow Sphere Stackings) and non-metallic materials (Ceramic Matrix Composites and Ultra High Temperature Composites) will be evaluated. Combined aero-thermal-structural experiments will test various materials as specimens and realistic shapes at extreme conditions representative for high flight Mach numbers. Both static and cyclic tests at low and high temperatures are planned including the evaluation of their durability in terms of long duration exposure to the harsh flight conditions. The materials assigned to dedicated engine components will be exposed to realistic combustion environments. These will be combined with passive or active cooling technologies developed in ATLLAS-I.'