• DocumentCode
    1046024
  • Title

    Hypersonic flight [scramjet aircraft propulsion]

  • Author

    Guizzo, Erico

  • Volume
    41
  • Issue
    1
  • fYear
    2004
  • Firstpage
    66
  • Abstract
    Current turbojet engines cannot propel an aircraft to hypersonic speeds -their spinning shafts and compressors would simply collapse. To solve this problem, groups in the United States, Japan, Australia, and other countries are working on a propulsion system that burns fuel combined with air flowing at supersonic speeds through the engine, which is essentially a metallic funnel, with no moving parts. These so-called supersonic combustion ramjet (scramjet) engines, outlined in this article, could in theory propel an aircraft to Mach 10 and eventually even more.
  • Keywords
    hypersonic flow; jet engines; supersonic flow; fuel/air burning propulsion system; hypersonic speeds; metallic funnel; no moving parts; scramjet aircraft propulsion; supersonic combustion ramjet; turbojet engines; Aircraft propulsion; Australia; Combustion; Compressors; Engines; Fuels; Shafts; Spinning;
  • fLanguage
    English
  • Journal_Title
    Spectrum, IEEE
  • Publisher
    ieee
  • ISSN
    0018-9235
  • Type

    jour

  • DOI
    10.1109/MSPEC.2004.1317885
  • Filename
    1317885