A series of computer codes were developed to predict solid rocket motor produced contamination to spacecraft sensitive surfaces. Subscale and flight test data have confirmed some of the analytical results. Application of the analysis tools to a typical spacecraft has provided early identification of potential spacecraft contamination problems and provided insight into their solution; e.g., flight plan modifications, plume or outgassing shields and/or contamination covers.


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    Title :

    IUS solid rocket motor contamination prediction methods


    Contributors:


    Publication date :

    1980-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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