Protective enclosure for a camera, located on the exhaust stream of a rocket engine, permits continuous recording of erosion processes of materials used in nozzle throat structures. The system uses a standard camera in a water-cooled, pressurized enclosure having a unique, inert gas-swept viewing duct.


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    Titel :

    Rocket engine nozzle photographic system


    Beteiligte:
    Bailey, R. L. (Autor:in) / Tibbitts, W. C. (Autor:in)

    Erscheinungsdatum :

    1968-04-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rocket Engine Nozzle Concepts

    Hagemann, G. / Immich, H. / Nguyen, T. et al. | British Library Conference Proceedings | 2004


    Rocket Engine Nozzle Concepts

    Popp, Michael / Hulka, James / Yang, Vigor et al. | AIAA | 2004


    Theoretical liquid rocket engine nozzle flow fields

    MCAMIS, R. / LANKFORD, D. / PHARES, W. | AIAA | 1992


    Inviscid Nozzle for Aerospike Rocket Engine Application

    Bogoi, Alina ;Rugescu, Radu D. ;Misirliu, Valentin Ionut | Trans Tech Publications | 2015


    Photographic Investigation of Combustion in a Two-dimensional Transparent Rocket Engine

    Bellman, Donald R / Humphrey, Jack C / Male, Theodore | NTRS | 1953