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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    Titel :

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


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Bhide, R. S. (Autor:in) / Kaila, V. K. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1994



    Erscheinungsdatum :

    01.06.1994




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Precise Relative Orbit Estimation of INSAT Missions

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