Small launch vehicles present an economically viable method for placing small satellites into orbit. These launch vehicles would be even more attractive to satellite customers if they could provide a softer ride to orbit. Passive whole-spacecraft vibration isolation systems have been developed for small launch vehicles to greatly reduce the dynamic launch loads. To date, two types of isolation systems have been designed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multi-axis whole-spacecraft vibration isolation for small launch vehicles


    Beteiligte:

    Kongress:

    Smart Structures and Materials 2001: Damping and Isolation ; 2001 ; Newport Beach,CA,United States


    Erschienen in:

    Erscheinungsdatum :

    02.07.2001





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Whole-Spacecraft Vibration Isolation on Small Launch Vehicles

    P. S. Wilke / C. D. Johnson / P. J. Grosserode et al. | NTIS | 2000


    Whole-spacecraft vibration isolation on small launch vehicles

    Wilke, Paul S. / Johnson, Conor D. / Grosserode, Patrick J. et al. | SPIE | 2000


    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


    Whole-Spacecraft Passive Launch Isolation

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