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HEXAFLY-INT

Financiado

Cerrado

High Speed Experimental Fly Vehicles International

The HEXAFLY-INT project aims to flight test an experimental vehicle above Mach 7 to verify its potential for a high aerodynamic efficiency during a free-flight while guaranteeing a large internal volume. The feasibility for a 3m l... ver más

30/09/2019

MINISTERE DE L'ENS...

12M€

Presupuesto del proyecto: 12M€

Líder del proyecto

MINISTERE DE L'ENSEIGNEMENT SUPERIEUR ET DE... No se ha especificado una descripción o un objeto social para esta compañía.

Fecha límite participación Sin fecha límite de participación.

Ver 10 Participantes

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2019-09-30 No tenemos la información de la convocatoria

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10 Participantes

MINISTERE DE L'ENSEIGNEMENT...

0.00€ | Lider

VON KARMAN INSTITUTE FOR FLU...

N.D. | Participante

USTUTT

N.D. | Participante

CIRA

N.D. | Participante

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Líder del proyecto

MINISTERE DE L'ENSEIGNEMENT SUPERIEUR ET DE... No se ha especificado una descripción o un objeto social para esta compañía.

Presupuesto del proyecto 12M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The HEXAFLY-INT project aims to flight test an experimental vehicle above Mach 7 to verify its potential for a high aerodynamic efficiency during a free-flight while guaranteeing a large internal volume. The feasibility for a 3m long vehicle was demonstrated during the European L0 precursor project HEXAFLY. Its realization will now be enabled on an international scale underlining the need for global cooperation in case of a future deployment of a high-speed cruiser. This flight opportunity will increase drastically the Technology Readiness Level of developments realized in previous high-speed EC projects such as ATLLAS I & II and LAPCAT I & II. The different technologies and methodologies which need experimental flight testing at high speed are grouped around the major axes of HEXAFLY-INT: 1. High-Speed Vehicle Concepts 2. High-Speed Aerodynamics 3. High-Temperature Materials and Structures 4. High-Speed Flight Control 5. High-Speed Environmental Impact To realize this experimental flight test, different consecutive steps are planned each followed by a critical review together with international partners: – updated of the mission profile based upon the feasibility study – a detailed design of a high-speed experimental flight vehicle – selection and manufacturing of ground-tested technologies and systems – assembly, integration and testing of the experimental flight test vehicle – identification and procurement of the most promising flight platform(s) The design of the experimental high-speed cruise vehicle will be the main driver and challenge in this project with following scientific objectives: - an aerodynamic balance at a cruise Mach number higher than 7 - an integrated conceptual design demonstrating a combined volumetric and aerodynamic efficiency - making maximum use of developed advanced high-temperature materials

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