The effort was confined primarily to a review of the existing Lockheed reports, assembly of available physical properties of the propellants and initiating a simplified analysis to give the order of magnitude values as an aid to specifying the important sources of forces resulting from heat transfer. (Author)


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    Titel :

    Study of Forces on Propellants Due to Heat Transfer Influencing Propellant Temperature in a Recovery Type Vehicle


    Erscheinungsdatum :

    1962


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch