Afterburner, developed by Continental Aviation, to improve performance of target drone aircraft uses mixture of triethylaluminum and trimethylaluminum to permit operation at combustion velocities considerably higher than those encountered in regular JP-4 afterburners; properties of fuels selected; nozzle ejection system and ignition; details of drone fuel system consisting of fuel tank, nitrogen bottle, fuel control and sequencing control; safety features.


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    Titel :

    Development of pyrophoric fuel thrust augmenter for J69 engine


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Bay, D.G. (Autor:in) / Hill, J.H. (Autor:in)

    Kongress:

    SAE Meeting ; 1960 Afterburners



    Erscheinungsdatum :

    1960


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    DEVELOPMENT OF A PYROPHORIC FUEL THRUST AUGMENTER FOR THE J69 ENGINE

    BAY, D. G. / HILL, J. H. | SAE Technical Papers | 1960


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    Panchenko, V. I. / Bikbulatov, R. R. | Springer Verlag | 2012


    On calculation of ideal thrust augmenter

    Panchenko, V. I. / Bikbulatov, R. R. | Online Contents | 2012


    Experimental investigation of a nonsteady flow thrust augmenter

    Amin, Sameh M. / Garris, Charles A. | AIAA | 1996


    Inlet and Internal Aerodynamics of a VTOL Thrust Augmenter

    J. L. Loth / S. Chandra / E. H. Gibbs | NTIS | 1976