In study carried out by Northrop Space Laboratories, variety of structural configurations successfully self-sealed following penetrations at speeds from 8000 to 20,000 fps; more successful sealants exhibit high damping and energy dissipation when compared with less successful materials; in unique application of theory of viscoelasticity, models of material response are proposed, and qualitative description of successful operation is advanced; material property data, results of hypervelocity perforations of elastomers and complete panels are presented.


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    Titel :

    Self-sealing spacecraft structures in meteoroid environment


    Weitere Titelangaben:

    AIAA -- Tech Paper


    Beteiligte:

    Kongress:

    Meeting of the 2nd AIAA -- Manned Space Flight ; 1963 Meteor impact



    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Meteoroid environment and its consequences to spacecraft structures

    Christman, D.R. / McMillan, A.R. | Engineering Index Backfile | 1966


    Meteoroid protection for spacecraft structures final report

    Bristow, R. J. / Lundeberg, J. F. / Stern, P. H. | NTRS | 1965


    Meteoroid Protection for Spacecraft Structures Final Report

    R. J. Bristow / J. F. Lundeberg / P. H. Stern | NTIS | 1965