RIVET JOINT is a USAF Electronic Systems Command (ESC) airborne (RC-135) reconnaissance system. The objectives of an ongoing modernization program are to improve mission capability and manpower utilizaiton through use of state-of-the-art computer technology and surveillance equipment. A prototype modernized system recently underwent testing and evaluation in the real-world operational environment. ESC/SD requested that the USAF School of Aerospace Medicine (USAFSAM/VN) evaluate the impact of the system on operator stress and fatique. Psychobiological data were systematically collected from 13 operators over 6 consecutive days, including two 8-hour airborne test missions. The subjective fatigue and physiological cost associated with the test missions were moderate and did not suggest compromises in performance and safety. The operators were fully recovered from each of the test missions after an extended postmission night of sleep. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Mission Crew Fatigue during RIVET JOINT Block II Demonstration/Evaluation


    Beteiligte:
    W. F. Storm (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    MSFC Skylab Crew Systems Mission Evaluation

    Marshall Space Flight Center | NTRS | 1974


    METHOD FOR MANUFACTURING RIVET JOINT STRUCTURE, RIVET JOINT STRUCTURE AND AUTOMOBILE COMPONENTS

    FUJIMOTO HIRONORI / IMAMURA TAKASHI / MATSUI SHO | Europäisches Patentamt | 2021

    Freier Zugriff

    METHOD FOR MANUFACTURING RIVET JOINT STRUCTURE, RIVET JOINT STRUCTURE AND AUTOMOBILE COMPONENTS

    FUJIMOTO HIRONORI / IMAMURA TAKASHI / MATSUI SHO | Europäisches Patentamt | 2021

    Freier Zugriff

    METHOD FOR MANUFACTURING RIVET JOINT STRUCTURE, RIVET JOINT STRUCTURE AND AUTOMOBILE COMPONENTS

    FUJIMOTO HIRONORI / IMAMURA TAKASHI / MATSUI SHO | Europäisches Patentamt | 2021

    Freier Zugriff