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Achievements obtained within ATLLAS-II on Aero-Thermal Loaded Material Investigations for High-Speed Vehicles

Steelant, Johan und Dalenbring, Mats und Kuhn, Markus und Bouchez, Marc und von Wolfersdorf, Jens (2017) Achievements obtained within ATLLAS-II on Aero-Thermal Loaded Material Investigations for High-Speed Vehicles. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Seiten 1-60. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6.-9. März 2017, Xiamen, China. doi: 10.2514/6.2017-2393.

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Offizielle URL: https://doi.org/10.2514/6.2017-2393

Kurzfassung

The co-founded FP7 EC project ATLLAS-II had as objectives the identification and assessment of advanced lightweight and high-temperature resistant materials for high-speed vehicles up to Mach 6. The material requirements were defined through an in-depth feasibility study of a Mach 5-6 vehicle. The consortium could build upon a 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, a multi-disciplinary optimization and experimental testing resulted into a detailed layout of a high-speed vehicle. Special attention was given to alleviate sonic boom and emissions at high altitudes. Throughout the design process, the aero-thermal loads defined the requirements for the proposed materials and cooling techniques needed for both the airframe and propulsion components. The former focused on sharp leading edges, intakes and skin materials each coping with different external aero-thermal loads. The latter were 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 Ceramics) were evaluated. Combined aero-thermal-structural experiments tested various materials at extreme conditions representative for high flight Mach numbers. Both static and cyclic tests at low and high temperatures were performed including the evaluation of their durability in terms of long duration exposure to the harsh flight conditions. The materials assigned to dedicated engine components were exposed to realistic combustion environments. These were combined with passive or active cooling technologies developed in ATLLAS-I.

elib-URL des Eintrags:https://elib.dlr.de/120616/
Dokumentart:Konferenzbeitrag (Vortrag)
Zusätzliche Informationen:AIAA 2017-2393
Titel:Achievements obtained within ATLLAS-II on Aero-Thermal Loaded Material Investigations for High-Speed Vehicles
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Steelant, JohanESA-ESTEC, NLNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Dalenbring, MatsTotalförsvarets forskningsinstitut - FOINICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Kuhn, MarkusMarkus.Kuhn (at) dlr.dehttps://orcid.org/0000-0002-0633-2327NICHT SPEZIFIZIERT
Bouchez, MarcMBDA, FNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
von Wolfersdorf, JensInstitute of Aerospace Thermodynamics, Universität StuttgartNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:9 Mai 2017
Erschienen in:21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.2514/6.2017-2393
Seitenbereich:Seiten 1-60
Status:veröffentlicht
Stichwörter:ATLLAS II, HIGH-SPEED VEHICLE DESIGN, CERAMIC MATRIX COMPOSITE (CMC), COMBINED CYCLE CONCEPT, EXPERIMENTS, HYPERSONIC FLOW, HYPERSONIC PROPULSION, LIFE TIME ASSESSMENT, MATERIALS, MULTIDISCIPLINARY DESIGN OPTIMISATION (MDO), SONIC BOOM, TITANIUM MATRIX COMPOSITE (TMC), ULTRA HIGH TEMPERATURE CERAMIC (UHTC)
Veranstaltungstitel:21st AIAA International Space Planes and Hypersonics Technologies Conference
Veranstaltungsort:Xiamen, China
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:6.-9. März 2017
Veranstalter :AIAA
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Raumfahrzeugsysteme - Konzepte und Entwurf (alt), R - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Standort: Stuttgart
Institute & Einrichtungen:Institut für Bauweisen und Strukturtechnologie > Raumfahrt - System - Integration
Hinterlegt von: Kuhn, Markus
Hinterlegt am:03 Jul 2018 10:21
Letzte Änderung:20 Jun 2021 15:51

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