One of the most severe environment that a satellite will be subjected to during its lifetime will occur during qualification testing and launch. This paper summarizes the results and status of research efforts in the area of satellite isolation from the launch environment. The objective of this effort was to reduce the launch induced-dynamic acceleration of the satellite by insertion of a passive isolator. Isolation issues involving the use of passive elements and launch vehicle system-level requirements will be discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Passive Isolation Systems for Launch Vehicles


    Beteiligte:

    Kongress:

    Fifth International Conference on Space ; 1996 ; Albuquerque, New Mexico, United States



    Erscheinungsdatum :

    1996-07-19




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Passive Isolation Systems for Launch Vehicles

    Fosness, E. R. / Wilke, P. S. / Johnson, C. D. et al. | British Library Conference Proceedings | 1996


    Whole-Spacecraft Passive Launch Isolation

    Paul S. Wilke / Conor D. Johnson / Eugene R. Fosness | AIAA | 1998


    Whole-Spacecraft Passive Launch Isolation

    P. S. Wilke / C. D. Johnson / E. R. Fosness | NTIS | 1997


    Whole-Spacecraft Passive Launch Isolation

    P. S. Wilke / C. D. Johnson / E. R. Fosnees | NTIS | 1998


    Whole-spacecraft passive launch isolation

    Wilke, Paul / Johnson, Conor / Fosness, Eugene | AIAA | 1997