• DocumentCode
    1231249
  • Title

    Heat-Shield Ablation and Sublimation Determinations through Radioisotope Techniques

  • Author

    Brandon, George W. ; Davis, William G.

  • Author_Institution
    NASA Manned Spacecraft Center Houston, Texas
  • Issue
    2
  • fYear
    1965
  • fDate
    6/1/1965 12:00:00 AM
  • Firstpage
    278
  • Lastpage
    283
  • Abstract
    A technique has been developed for the determination of heat-shield sublimation (char) and surface recession (ablation) during an atmospheric reentry. A radioactive "line" source embedded in the heat-shield material sublimes and ablates at the same rate as the heat shield. Decreases in source activity are monitored by miniaturized nuclear counters. Accuracies exceeding 90 percent are obtainable. The technique provides a continuous indication of char and ablation rates.
  • Keywords
    Aerospace materials; Automotive engineering; Protection; Radioactive materials; Space exploration; Space heating; Space vehicles; Temperature sensors; Terrestrial atmosphere; Thermal sensors;
  • fLanguage
    English
  • Journal_Title
    Aerospace, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0536-1516
  • Type

    jour

  • DOI
    10.1109/TA.1965.4319813
  • Filename
    4319813