• Home
  • Current congress
  • Public Website
  • My papers
  • root
  • browse
  • IAC-14
  • A2
  • 3
  • paper
  • PerWaves: Towards a Spaceflight Experiment to Realize Discrete Combustion Waves

    Paper number

    IAC-14,A2,3,1,x27132

    Author

    Prof. Andrew Higgins, McGill University, Canada

    Coauthor

    Mr. Alex Wright, McGill University, Canada

    Coauthor

    Dr. Samuel Goroshin, Canada

    Coauthor

    Dr. Francois-David Tang, ESA/ESTEC, The Netherlands

    Coauthor

    Mr. Antonio Verga, European Space Agency (ESA), The Netherlands

    Coauthor

    Mr. Andreas Schütte, Astrium Space Transportation, Germany

    Coauthor

    Mr. Burkhard Schmitz, Astrium Space Transportation, Germany

    Year

    2014

    Abstract
    Study of the propagation of reactive waves in suspensions of fuel particulates in an oxidizing atmosphere has long been a motivation for microgravity combustion research, due to the necessity of microgravity both to create the suspensions without settling and to eliminate buoyancy-induced disruption of the flame.  Recent theoretical and experimental investigations, however, have suggested that a novel mode of propagation, namely, discrete combustion waves, can be realized in microgravity at the limit of rapid heat release from point-like energy sources.  In this mode, the propagation of the wave is limited by particle-to-particle diffusion rather than the global energy release rate, giving rise to statistical, percolation-like waves (“PerWaves”).  This model of reactive wave propagation has been conjectured to occur in a variety of settings, from biological to astrophysical, yet a simple experimental realization of a system that can be directly visualized has yet to be demonstrated.  The system studied here is a fuel that reacts predominately in the condensed phase (iron) in a gaseous oxidizer with low thermal diffusivity (oxygen/xenon mixture).  This paper will review progress on the study of discrete combustion waves, including recent parabolic flight data and development of hardware and diagnostics in preparation for a sounding rocket flight that should permit the first unambiguous realization of the discrete mode of reactive wave propagation.
    Abstract document

    IAC-14,A2,3,1,x27132.brief.pdf

    Manuscript document

    IAC-14,A2,3,1,x27132.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.