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  • Optical degradation and recovery of multilayer insulation in a simulated GEO environment

    Paper number

    IAC-18,A6,IP,40,x46936

    Author

    Dr. Daniel Engelhart, United States, Assurance Technology Corporation

    Coauthor

    Mr. Jordan Maxwell, United States, Colorado Center for Astrodynamics Research, University of Colorado

    Coauthor

    Mr. Miles Bengtson, United States, Colorado Center for Astrodynamics Research, University of Colorado

    Coauthor

    Dr. Elena Plis, United States

    Coauthor

    Dr. Russell Cooper, United States, Air Force Research Laboratory (AFRL)

    Coauthor

    Dr. Heather Cowardin, United States, Jacobs Engineering

    Coauthor

    Dr. Dale Ferguson, United States, Air Force Research Laboratory (AFRL)

    Coauthor

    Dr. Stephanie Schieffer, United States, Air Force Research Laboratory (AFRL)

    Coauthor

    Mr. Ryan Hoffmann, United States

    Year

    2018

    Abstract
    Ground- and space-based optical observations of space objects rely on knowledge about how spacecraft materials interact with light and how that interaction changes as a function of space weather exposure. In polymers, the changes in optical signature occur due to surface degradation, leading to altered reflectivity, and due to radiation induced chemical modification, leading to an alteration of a material’s absorption/transmission properties. Electrons can be expected to primarily alter the bulk of the material with minimal effect on surface morphology due to the nature of energy deposition. The optical fingerprint of commonly used spacecraft surface materials changes continuously under exposure to high energy electrons, the primary damaging species in geostationary Earth orbit (GEO). Laboratory observations have also shown that these changes in a material’s optical signature are to some degree transient. This work investigates the rate and degree of “optical healing” in vacuum for electron damaged polyimide (Kapton-H®), a major component in many variations of multilayer insulation (MLI). Characterization of optical damage as a function of electron exposure and optical healing as a function of time in vacuum represents a major step toward a predictive model for optical characterization of space objects. The results of this investigation will find use in the space environmental remediation community for characterization of high area to mass ratio (HAMR) objects as MLI fragments comprise a large portion of HAMR space debris.
    Abstract document

    IAC-18,A6,IP,40,x46936.brief.pdf

    Manuscript document

    IAC-18,A6,IP,40,x46936.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.