A unique separation and jettison system for the ascent fairing and a staging system for the apogee motor of the first Indian satellite launch vehicle are described. Design features, development problems, and mission constraints are discussed in addition to the solutions adopted. A qualification summary is included for each system, and flight results obtained from SLV-3 launches are described.


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    Title :

    Separation and Staging Mechanisms for the Indian SLV-3 Launch Vehicle


    Contributors:


    Publication date :

    1984-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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