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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    Title :

    Rocket engine nozzle photographic system


    Contributors:

    Publication date :

    1968-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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