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High-Speed Experimental Fly Vehicles

Project

HEXAFLY - High-Speed Experimental Fly Vehicles


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/10/2012,
End date: 31/03/2014

Status: Finished
Funding details:
Total cost:
€829 898
EU Contribution:
€599 960

Overview

Objectives:

The HEXAFLY project aims to mature an experimental high-speed self-propelled vehicle in combination with several multi-disciplinary technologies. By this approach, the grounds for a future flight test will be prepared and potential technological risks identified in time. This potential will increase drastically the Technology Readiness Level (TRL) of developments realized in previous high-speed aeronautical projects on national and European level 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 six major axes of HEXAFLY:

  1. High-Speed Vehicle Concepts
  2. High-Speed Aerodynamics
  3. High-Speed Propulsion
  4. High-Temperature Materials and Structures
  5. High-Speed Flight Control
  6. High-Speed Environmental Impact

Methodology:

To mature this experimental flight testing, a scientific mission profile will be defined followed by a proof-of-concept based upon:

  • A preliminary design of a high-speed experimental flight vehicle covering the six major axes
  • Selection and integration of available ground-tested technologies
  • Identification of the most promising flight platform(s)

This allows to address the following items for a follow-up project:

  • Identification of potential technological barriers
  • Assessment of the overall ROM-costs
  • The progress and potential of technology development at a higher TRL

The design of the experimental high-speed cruise vehicle design will be the main driver and challenge in this project with following scientific objectives:

  • A positive aero-propulsive balance at a cruise Mach number of 8
  • An integrated conceptual design demonstrating a combined propulsive and aerodynamic efficiency
  • Making maximum use of earlier developed advanced high-temperature materials and/or structures
  • An evaluation of the sonic boom impact by deploying dedicated ground measurement equipments

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