Glass Transition Temperature (T g) 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 g) measurements on travel coupons of Nose Cone Radome for Jaguar Maritime Aircraft. Technical Report. NAL, Bangalore.

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    Abstract

    This report presents the glass transition temperature (T g) 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 from the base ring of the fully cured radomes were taken for Tg measurements by DSC and are presented in this report . The Tg of 5 SOF test articles were with in the range of 155 to 160 °C .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Composite materials; post cure; Tempo oven; DSC, RTM
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 05 Jul 2012 10:01
    Last Modified: 05 Jul 2012 10:01
    URI: http://nal-ir.nal.res.in/id/eprint/10511

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