Advanced flight vehicles operating at acceleration loads beyond human functional capabilities require a new reclining seat design. An ejection seat compatible with this requirement must provide safe ejection and aircraft clearances under high-G conditions as well as the requirements associated with high dynamic pressures and low altitudes. Design criteria and interface requirements have been established. Ejection seat subsystems have been developed and seat design concepts generated to meet criteria and interface requirements. Candidate seat concepts have been analyzed to determine cockpit integration effects, accelerations, ejection clearances, escape performance, structural requirements and weights. A final design concept has been selected to meet all requirements of an ejection seat for high-G escape. The final report includes a parametric study of tail clearances and discusses technical design details and conclusions of the work performed. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ejection Seat for High G Escape


    Beteiligte:
    O. E. Howland (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    184 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Multi-seat escape system and ejection seat sequencer

    STEVE HOLSTINE / LUIS G INTERIANO / JEFFREY BENJAMIN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Multi-seat escape system and ejection seat sequencer

    HOLSTINE STEVE / INTERIANO LUIS G / BENJAMIN JEFF et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    MULTI-SEAT ESCAPE SYSTEM AND EJECTION SEAT SEQUENCER

    HOLSTINE STEVE / INTERIANO LUIS G / BENJAMIN JEFF et al. | Europäisches Patentamt | 2023

    Freier Zugriff


    CFD Analysis of Ejection Seat Escape Systems

    Przekwas, A.J. / Ayoub, P. / Habchi, S.D. et al. | SAE Technical Papers | 1992