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TRIMIS

High-Speed Experimental Fly Vehicles - International

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€11 544 935
EU Contribution
€5 000 000
Project Acronym
HEXAFLY-INT
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
FP7-AAT-2013-RTD-HIGH-SPEED
Link to CORDIS
Objectives

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:

  • update 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

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
The European Commission
Type of funding
Public (EU)
Specific funding programme
FP7-TRANSPORT

Partners

Lead Organisation
Organisation
European Space Agency
Address
24 Rue Du General Bertrand, 75007 Paris, France
EU Contribution
€693 055
Partner Organisations
Organisation
Tecnosistem Spa
Address
Vico Ii S Nicola Alla Dogana 9, 80133 Napoli, Italy
EU Contribution
€2 914 534
Organisation
Tecnosistem Spa
Address
Vico Ii S Nicola Alla Dogana 9, 80133 Napoli, Italy
EU Contribution
€241 500
Organisation
Marotta Srl
Address
Via G.marconi 18/a, 80040 Cercola Na, Italy
EU Contribution
€300 000
Organisation
Marotta Srl
Address
Via G.marconi 18/a, 80040 Cercola Na, Italy
EU Contribution
€401 250
Organisation
Techno System Development Srl
Address
Zona Industriale San Martino - Via Provinciale Pianura - 2 Int.23, 80078 Pozzuoli (Na), Italy
EU Contribution
€2 594 337
Organisation
Techno System Development Srl
Address
Zona Industriale San Martino - Via Provinciale Pianura - 2 Int.23, 80078 Pozzuoli (Na), Italy
EU Contribution
€422 062
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€3 815 410
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€672 830
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€2 852 252
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€1 149 295
Organisation
Airbus
Address
2 ROND POINT EMILE DEWOITINE, 31700 BLAGNAC, France
Organisation website
EU Contribution
€1 824 560
Organisation
Airbus
Address
2 ROND POINT EMILE DEWOITINE, 31700 BLAGNAC, France
Organisation website
EU Contribution
€166 500
Organisation
Centro Italiano Ricerche Aerospaziali Scpa
Address
Via Maiorise s/n, 81043 CAPUA (CE), Italy
Organisation website
EU Contribution
€1 872 081
Organisation
Centro Italiano Ricerche Aerospaziali Scpa
Address
Via Maiorise s/n, 81043 CAPUA (CE), Italy
Organisation website
EU Contribution
€1 153 225
Organisation
Gas Dynamics Ltd
Address
22 Empress Avenue, Farnborough, GU14 8LX, United Kingdom
EU Contribution
€15 617 318
Organisation
Gas Dynamics Ltd
Address
22 Empress Avenue, Farnborough, GU14 8LX, United Kingdom
EU Contribution
€75 000
Organisation
Institut Von Karman De Dynamique Des Fluides
Address
Chaussee De Waterloo 72, 1640 Rhode Saint Genese, Belgium
EU Contribution
€2 883 657
Organisation
Institut Von Karman De Dynamique Des Fluides
Address
Chaussee De Waterloo 72, 1640 Rhode Saint Genese, Belgium
EU Contribution
€17 783
Organisation
Universitaet Paderborn
Address
Warburger Strasse 100, 33098 Paderborn, Germany
Organisation website
EU Contribution
€4 957 469
Organisation
Universitaet Paderborn
Address
Warburger Strasse 100, 33098 Paderborn, Germany
Organisation website
EU Contribution
€7 500

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Hypersonic aircraft technology
Development phase
Validation
Technology Theme
Aircraft design and manufacturing
Technology
High temperature structural materials
Development phase
Validation
Technology Theme
Aircraft design and manufacturing
Technology
High speed flight control
Development phase
Validation
Technology Theme
Aircraft design and manufacturing
Technology
Hypersonic aircraft technology
Development phase
Validation

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