The interferometric holography method was used to visualize adhesion defects between bonded materials simulating those existing in rocket propulsion systems. Nondestructive loads were applied, mostly pneumatic and thermal, to exhibit these defects. The nature and thickness of materials are influencing factors the effects of which were determined. Possible application to industrial tests is outlined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Holographic Testing of Rocket Combustion Chambers Controle des Propulseurs Par Holographie


    Beteiligte:
    P. Smigielski (Autor:in) / A. Stimpfling (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Combustion chambers for rocket engines

    Baxter, A.D. | Engineering Index Backfile | 1956



    Innovative Cooling for Rocket Combustion Chambers

    Peichl, Jonas / Schwab, Andreas / Selzer, Markus et al. | Springer Verlag | 2020

    Freier Zugriff


    Rocket Combustion Chambers Resist Thermal Fatigue

    Kazaroff, John M. / Jankovsky, Robert S. / Pavli, Albert J. | NTRS | 1995