A pilot operational ISHM capability has been implemented for the E-2 Rocket Engine Test Stand (RETS) and a Chemical Steam Generator (CSG) test article at NASA Stennis Space Center. The implementation currently includes an ISHM computer and a large display in the control room. The paper will address the overall approach, tools, and requirements. It will also address the infrastructure and architecture. Specific anomaly detection algorithms will be discussed regarding leak detection and diagnostics, valve validation, and sensor validation. It will also describe development and use of a Health Assessment Database System (HADS) as a repository for measurements, health, configuration, and knowledge related to a system with ISHM capability. It will conclude with a discussion of user interfaces, and a description of the operation of the ISHM system prior, during, and after testing.


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    Title :

    Integrated System Health Management (ISHM) Implementation in Rocket Engine Testing


    Contributors:

    Conference:

    AIAA Infotech@Aerospace 2011 ; 2011 ; Saint Louis, MO, United States


    Publication date :

    2010-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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