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    Deployable Shroud for the International X-Ray Observatory (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: A document describes the design of a lightweight (between 100 to 200 kg), light-tight shroud of about 3.9 meters in diameter that could be stowed into a very small volume, and be deployed to 12 meters. The shroud will consist of two concentric multi-layer blankets (MLIs) that are constructed in an accordion shape.
    Keywords: Spacecraft Design, Testing and Performance
    Type: GSC-15779-1 , NASA Tech Briefs, November 2009; 37
    Format: application/pdf
    Location Call Number Expected Availability
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