This paper presents data from the thermostructural testing of tape-wrapped carbon phenolic. This work has been performed with the use of a plasma torch and loading device in an effort to study the anomalous erosion characteristicfs of that seen in the Space Shuttle Solid Rocket Motor Nozzle STS-8A. Testing is conducted in an effort to determine conditions or parameters involved in this mode of failure.


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    Titel :

    Plasma torch testing for thermostructural evaluation of rocket motor nozzle materials


    Beteiligte:

    Erscheinungsdatum :

    1989-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Plasma torch testing for thermostructural evaluation of rocket motornozzle materials

    PRINCE, ANDREW / BUNKER, ROBERT / LAWRENCE, TIM | AIAA | 1989



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    MELCHIOR, A. / POULIQUEN, M. / SOLER, E. | AIAA | 1987


    Integrity and testing concerns of thermostructural materials

    Raynal, R. / Centre national d'etudes spatiales | British Library Conference Proceedings | 1992


    Numerical simulation of the dynamic thermostructural response of a composite rocket nozzle throat

    Morozov, E.V. / Beaujardiere, J.F.P. Pitot de la | Tema Archiv | 2009