The Orion space vehicle is designed to requirements for both direct attachment and indirect effects of lightning. Both sets of requirements are based on a full threat 200kA strike, in accordance with constraints and guidelines contained in SAE ARP documents applicable to both commercial and military aircraft and space vehicles. This paper describes the requirements as levied against the vehicle, as well as the means whereby the design shows full compliance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lightning Protection for the Orion Space Vehicle


    Beteiligte:
    Scully, Robert (Autor:in)

    Kongress:

    AIAA Atmospheric and Space Environments Conference ; 2015 ; Dallas, TX, United States


    Erscheinungsdatum :

    2015-06-22


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Lightning Protection for the Orion Space Vehicle (AIAA 2015-3320)

    Scully, Robert C. | British Library Conference Proceedings | 2015


    Crew Exploration Vehicle (CEV) (Orion) Occupant Protection

    Currie-Gregg, Nancy J. / Gernhardt, Michael L. / Lawrence, Charles et al. | NTRS | 2016