The Crew Exploration Vehicle (CEV) was intended to be the next-generation human spacecraft for the Constellation Program. The CEV Isolator Strut mechanism was designed to mitigate loads imparted to the CEV crew caused by the Thrust Oscillation (TO) phenomenon of the proposed Ares I Launch Vehicle (LV). The Isolator Strut was also designed to be compatible with Launch Abort (LA) contingencies and landing scenarios. Prototype struts were designed, built, and tested in component, sub-system, and system-level testing. The design of the strut, the results of the tests, and the conclusions and lessons learned from the program will be explored in this paper.


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    Titel :

    Passive Thrust Oscillation Mitigation for the CEV Crew Pallet System


    Beteiligte:
    M. Sammons (Autor:in) / C. Powell (Autor:in) / J. Pellicciotti (Autor:in) / R. Buehrle (Autor:in) / K. Johnson (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch