Combined Altitude Temperature and Humidity Testing of the Solid State Flight Data Recorder (Ssfdr) for the Su-30 MKI Aircraft

Srihari, Shylaja and Revathi, A and Murugan, M. Sendil and Rao, RMVGK (2007) Combined Altitude Temperature and Humidity Testing of the Solid State Flight Data Recorder (Ssfdr) for the Su-30 MKI Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    The Solid State Flight Data Recorder (SSFDR) unit was subjected to CATH test in a Combined Altitude, Temperature and Humidity chamber. This unit was developed by M/S SLN Technologies Pvt Ltd Bangalore, for SU-30 MKI Aircraft to HAL,Korwa. This unit has LRU's namely, 1. Data Acquisition Unit(DAU), 2. Recorder Unit (RU) and 3. Control and Indication Unit (CIU). The CATH test was done as per MIL-STD 810F, Method 520.2. After conditioning, the functional test was carried out by the firm and the unit was handed over to them.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: CATH;SSFDR;SU-30 MKI;Aircraft
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division, Fibre Reinforced Plastics Division
    Depositing User: Mr Nisanth
    Date Deposited: 21 Jul 2011 10:05
    Last Modified: 21 Jul 2011 10:05
    URI: http://nal-ir.nal.res.in/id/eprint/9526

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