Study carried out by Lockheed Missiles and Space Co to develop and experimentally qualify theoretical performance model for nylon phenolic; mathematical treatment consists of description of individual depolymerization kinetics of two-component resin-fabric composite and quantitative analysis of decomposition products, and description of their chemical behavior as they diffuse to char surface; resulting theory and coefficients are applied in correlation of air-arc test data and flight data to establish validity of analysis procedures developed.


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    Titel :

    Thermal performance of heat shield composites during planetary entry


    Weitere Titelangaben:

    AIAA -- Tech Papers


    Beteiligte:
    Kratsch, K.M. (Autor:in) / Hearne, L.F. (Autor:in) / McChesney, H.R. (Autor:in)

    Kongress:

    AIAA -- Engineering Problems of Manned Interplanetary Exploration Meeting ; 1963 Radiation shielding



    Erscheinungsdatum :

    1963


    Format / Umfang :

    73 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    THERMAL PERFORMANCE OF HEAT SHIELD COMPOSITES DURING PLANETARY ENTRY

    KRATSCH, K. / HEARNE, L. / MCCHESNEY, H. | AIAA | 1963


    A Multifunctional Hot Structure Heat Shield Concept for Planetary Entry

    Walker, Sandra P. / Daryabeigi, Kamran / Samareh, Jamshid A. et al. | AIAA | 2015


    A Multifunctional Hot Structure Heat Shield Concept for Planetary Entry (AIAA 2015-3530)

    Walker, Sandra P. / Daryabeigi, Kamran / Samareh, Jamshid A. et al. | British Library Conference Proceedings | 2015


    Entry Performance of the Mercury Spacecraft Heat Shield

    Erb, R. B. / Jacobs, S. | NTRS | 1964