The high speed cameras were used to develop the new sounding rocket motor and to check the safety operation system. The new rocket motor was designed as a single stage rocket and its power was greater than the multi-stage K-9M rocket motor. The test combustion of this new type rocket engine was photographed by the high speed cameras to analyze the burning process. At the outside of rocket chamber, the cable which connect the detector of an engine nozzle with the telemeter system was fixed. To check the thero.,a1 influences of combustion flame to the cable, the thermo-tapes and high speed cameras were used Safety operation system was tested and photographed with high speed cameras using a S0-1510 model rocket.


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    Titel :

    High Speed Photographic Studies Of Rocket Engine Combustion


    Beteiligte:

    Kongress:

    15th Intl Congress on High Speed Photography and Photonics ; 1982 ; San Diego,United States


    Erschienen in:

    Erscheinungsdatum :

    01.03.1983





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Rocket engine nozzle photographic system

    Bailey, R. L. / Tibbitts, W. C. | NTRS | 1968


    Photographic investigation of combustion in two-dimensional transparent rocket engine

    Bellman, D.R. / Humphrey, J.C. / Male, T. | Engineering Index Backfile | 1953


    Photographic investigation of combustion in a two-dimensional transparent rocket engine

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


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

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