During the arctic test phase of the F-111D DT/E All-Weather Test Program, 24.0 hours of test time were accumulated in 12 test flights. Five of these flights were selected as being most representative of aircraft operation in an arctic environment. All available data obtained on these five flights are presented in this document as computer printouts.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    F-111D, DT and E Evaluation of Environmental Control, Airframe, Flight Control, and Secondary Power Subsystems. Appendix I


    Beteiligte:
    R. W. Olson (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    485 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    UH-1N Category II Airframe and Subsystems Evaluation

    H. M. Helmick / E. B. Russell | NTIS | 1971


    Optimization of flight-control, airframe system

    Ashkenas, I.L. / McRuer, D.T. | Engineering Index Backfile | 1960


    COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN

    Van Heerden, A. S. J. / Guenov, M. D. / Molina-Cristóbal, A. et al. | British Library Conference Proceedings | 2018