NASA is conducting a program which will establish a technology base for the orderly evolution of reusable space propulsion systems. As part of that program, NASA initiated a Structural Integrity and Durability effort for advanced high-pressure oxygen-hydrogen rocket engine technology. That effort focuses on the development of: (1) accurate analytical models to describe flow fields; aerothermodynamic loads; structural responses; and fatigue/fracture, from which life prediction codes can be evolved; and (2) advanced instrumentation with capabilities to verify the codes in an SSME-like environment as well as the potential for future use as diagnostic sensors for real-time condition monitoring of critical engine components.


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    Titel :

    Structural integrity and durability for Space Shuttle main engine and future reusable space propulsion systems


    Beteiligte:

    Kongress:

    Joint Propulsion Conference ; 1986 ; Huntsville, Alabama


    Erscheinungsdatum :

    1986-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch