• DocumentCode
    1019820
  • Title

    Technology of thermal hypervelocity launchers

  • Author

    Powell, J.R. ; Horn, F.L. ; Benenati, R. ; Lowrey, A.

  • Author_Institution
    Brookhaven National Laboratory, Upton, Long Island, NY, USA
  • Volume
    22
  • Issue
    6
  • fYear
    1986
  • fDate
    11/1/1986 12:00:00 AM
  • Firstpage
    1675
  • Lastpage
    1680
  • Abstract
    A new type of hypervelocity launcher is described, the Thermal Hypervelocity Launcher (THL). The THL uses stored thermal energy in a compact, lightweight particle bed heater to rapidly (milliseconds) heat a high pressure low molecular weight propellant (hydrogen or helium). The hot propellant then expands in a conventional barrel accelerating the projectile. The THL can achieve velocities up to -12 km/sec. The technology of the THL is described, including experiments on thermal-hydraulics of particle bed heaters. An experiment that will demonstrate THL operation with 100 gram projectiles at 3 km/sec is being attempted.
  • Keywords
    Propulsion; Thermal factors; Acceleration; Coolants; Fluid flow; Heat transfer; Helium; Hydrogen; Projectiles; Propulsion; Space heating; Valves;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/TMAG.1986.1064634
  • Filename
    1064634