This paper is the report of an analysis of the economic benefits of providing crashworthiness improvements within future Army utility helicopters. The analysis was performed for use in the Cost and Operational Effectiveness Analysis (COEA) for the Utility Tactical Transport Aircraft System (UTTAS). The analysis baseline is all UH-1H major aircraft accidents from January 1972 through December 1975. Major accident rates and losses due to accidents are derived for each COEA candidate aircraft. Losses are projected for a twenty year period of peacetime operation. Projections are derived based on each candidate's design features and the effectiveness of these features under the particular conditions in each UH-1H accident. Recommendations are made regarding use of accident losses within the UTTAS COEA and future similar studies. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Economic Benefits of Utility Aircraft Crashworthiness


    Beteiligte:
    J. E. Hicks (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft crashworthiness

    Saczalski, Kenneth | TIBKAT | 1975


    Aircraft crashworthiness

    Society of Automotive Engineers | TIBKAT | 1995


    Crashworthiness for Commercial Aircraft

    Tanner, A. J. / Commission of the European Communities | British Library Conference Proceedings | 1993


    TRANSFORMABLE AIRCRAFT CRASHWORTHINESS STRUCTURE

    PARK IL KYUNG / PARK SANG WOOK / KIM SUNG JOON | Europäisches Patentamt | 2016

    Freier Zugriff

    Emerging Technologies in Aircraft Crashworthiness

    Schoenbeck, A. C. / Schultz, M. R. / Research and Technology Organization | British Library Conference Proceedings | 2000