The Aircraft Crashworthiness Program Plan is designed to reduce or prevent aircraft occupants from incurring serious or fatal injuries in a 'survivable' crash impact accident by incorporating crashworthy design features into the initial stages of fixed-wing and rotary-wing aircraft development. It describes a 5-year development program for both airplanes and rotorcraft. It identifies five major subprogram areas for study and analysis to accomplish the program's goals: (1) Airframes; (2) Cabin safety; (3) Fuel system protection; (4) Emergency evacuation system; and (5) Standards, criteria, and procedures. The plan emphasizes use of available background data; development of analytical techniques; validation of analytical techniques; validation of data to determine feasibility/acceptability; and transmittal of appropriate data for consideration as the basis for regulation, standards, etc. The Federal Aviation Administration groups, other Government agencies/departments and industry organizations participating in this effort are identified. Program schedule with milestones is presented. Program management and funding requirements are also identified.


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    Titel :

    Engineering and Development Program Plan Aircraft Crashworthiness


    Beteiligte:
    C. A. Caiafa (Autor:in) / L. M. Neri (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    54 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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