A super insulated (multi layer insulation) heat shield has been designed and implemented for the 440 N Liquid Apogee Motor (LAM) of INSAT-2A and INSAT-2B satellites. The design had been arrived at its final configuration after a series of test and detailed analysis of the test data. An effective conductivity and emissivity for the shield insulation assembly was estimated and used for predicting the flight performance.


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    Title :

    Design and In-Orbit Performance of the Heat Shield Insulation for Liquid Apogee Motor of INSAT-2A and INSAT-2B


    Additional title:

    Sae Technical Papers


    Contributors:
    Bhide, R. S. (author) / Kaila, V. K. (author)

    Conference:

    International Conference On Environmental Systems ; 1994



    Publication date :

    1994-06-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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