Basic equipment to provide atmosphere environment required for aircraft or missiles involves: altitude loop capable of over 100,000-ft simulated altitude with about 120 tons of refrigerating capacity available and air drying system for humidity control; h-p air storage system with large compressors supplying it; small cold, hot and humidity chambers for debugging uses and isolation of noises and temperature.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Tightrope to tomorrow


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Hill, J.F. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting (Texas Section) ; 1958 Aircraft



    Erscheinungsdatum :

    1958


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    TIGHTROPE TO TOMORROW

    HILL, J. F. | SAE Technical Papers | 1958


    TightRope®

    Blessing, A. / Grützner, P. A. / Studier–Fischer, S. | British Library Online Contents | 2011


    Embraer walks WTO tightrope

    Online Contents | 1999


    SST-economic tightrope for airlines

    Macdonald, I.S. | Engineering Index Backfile | 1968