Glass Transition Temperature (T,) measurements on travel coupons of Nose Cone Radome for Jaguar Maritime Aircraft

Vanaja, A and Rao, Sandhya and Rao, RMVGK (2003) Glass Transition Temperature (T,) measurements on travel coupons of Nose Cone Radome for Jaguar Maritime Aircraft. Project Report. NAL, Bangalore.

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    Abstract

    This report presents the glass transition temperature (T,) on the travel coupons of nose cone radome for Jaguar Maritime Aircraft. The nose cone radome for jaguar Maritime Aircraft were fabricated by the Resin Injection Moulding (RIM) technique. The small cut out portions fiom the base ring of the fully cured radomes were taken for Tg measurements by DSC and are presented in this report. The T, of 5 SOF test articles were with in the range of 155 to 160°C.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Subjects: CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
    CHEMISTRY AND MATERIALS > Composite Materials
    Division/Department: Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division
    Depositing User: Mr Nisanth
    Date Deposited: 08 Jul 2011 16:25
    Last Modified: 08 Jul 2011 16:25
    URI: http://nal-ir.nal.res.in/id/eprint/9283

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