Launching the A-6A aircraft from the H-8 hydraulic catapult is feasible. Eight launches were conducted from the H-8 catapult and no aircraft deficiencies were observed. Launching the A-6A above 40,000 lb gross weight from the H-8 catapult is considered impractical because of the relatively high wind over the deck required.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Carrier Suitability Tests of the Model A-6A Aircraft


    Beteiligte:
    J. E. Ramsey (Autor:in) / W. R. Dixon (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Carrier Suitability Tests of the Rafale Aircraft in the United States

    Loftus, J. / Piekarski, B. / AIAA | British Library Conference Proceedings | 1994


    CARRIER SUITABILITY OF LAND-BASED AIRCRAFT

    Hernando, J.-L. / Martinez-Val, R. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2012


    Shuttle carrier aircraft flight tests

    Fulton, F. L., Jr. | NTRS | 1977


    Carrier suitability tests of the Rafale airplane in the United States

    Loftus, John / Piekarski, Bernard | AIAA | 1994