French Flight Test Program LEA Status

Abstract

The present lecture of the RTO-AVT-VKI course "HIGH SPEED PROPULSION: ENGINE DESIGN INTEGRATION AND THERMAL MANAGEMENT" is focused on the French flight experiment program called "LEA." French R&T effort for hypersonic airbreathing propulsion is focusing on needed technologies for the propulsion system and acquisition of aero-propulsive balance prediction capability. A large part of technology development effort can be led on ground and is currently dedicated to combustion chamber to ensure its performance and thermo-mechanical strength. On the contrary, it is mandatory to flight demonstrate capability to predict the aero-propulsive balance. In that view, MBDA and ONERA are leading the flight testing LEA program. Started in January 2003, the program will end in 2015 after 4 autonomous flight tests of an experimental vehicle in Mach number range 4 to 8. Guidelines for LEA vehicle and its propulsion system design have been validated in 2006 by a Preliminary Design Review. The running Phase 2 aims at getting a detailed design while validating the aero-propulsive configuration by a first free jet test series to be performed early in 2011. It led to a Critical Design Review performed in June/July 2009.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2010
Accession Number
ADA593055

Entities

People

  • Francois Falempin
  • Laurent Serre

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Chambers
  • Combustion
  • Combustion Chambers
  • Combustors
  • Engines
  • Flight Testing
  • Geometry
  • Ignition
  • Ignition Lag
  • Mach Number
  • Propulsion Systems
  • Simulations
  • Temperature Control
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.
  • Software Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow