Combined Altitude, Temperature and Humidity Testing of LCA Components (Line Replaement Unit, Function Sensor Display Unit, Stores Interface Box)

Shylaja, Srihari and Revathi, A and Sendil, Murugan and Rajendra Prakash, M and Navaneetha, S and Venkatasubramanyam, D.V (2008) Combined Altitude, Temperature and Humidity Testing of LCA Components (Line Replaement Unit, Function Sensor Display Unit, Stores Interface Box). Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    The LCA components (Line replacement Unit, Function Sensor Display Unit and Stores Interface Box) were subjected to CATH test in a Combined Altitude, Temperature and Humidity chamber. The CATH test was done as per MIL-STD 810 D and E for acceptance by end user. The LRU was developed by M/S Spectrum Infotech Pvt. Ltd; Bangalore for ADA, FSDU and SIB was developed by M/S Bharat Electronics Pvt Ltd. Bangalore. After conditioning, the functional test was carried out by the firm and the unit was handed over to the firm.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: CATH, Qualification, LRU, FSDU, SIB, LCA, Aircraft
    Subjects: CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
    Division/Department: Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division
    Depositing User: Ms Indrani V
    Date Deposited: 26 Mar 2012 10:25
    Last Modified: 26 Mar 2012 10:25
    URI: http://nal-ir.nal.res.in/id/eprint/10397

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