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    Personal information
    Contact information
    Candidate Profile
     Date Submitted:22-07-2011
     Last Modified:28-11-2012 (07:18)
    Job information
     Current job:Electrical Integration Engineer
     Employment Term:Temp/Contract
     Job location:Anywhere
     Date available:immediately
     Industry:Satellite Manufacturers and Subcontractors, Satellite Operators, , , Launch Systems
     KeywordsWorking as an Electrical Integrationto carrying out Assembly,Integration and Testing of Satellites . Harness Designing for spacecraft,Clean Room level Integration and Testing,Launch Pad Operations. Expert in Electrical Harness design using CATIA V5.



    Work Experience

    §  Total Experience

    3.4 Years


    §  Aerospace Experience

    4 Months(Till date)

    Model Based Definition (MBD) for Aircraft fuselage.

    §  Space Experience

    2 Years

    Spacecraft Assembly,Integration & Testing(AIT)&

    Electrical Harness design.

    §  Design Experience

    1 Year

    Designing the material for BHEL by 2D AutoCAD






    §  Unit Force Technologies

    (July 2012-Till date)





    INFOSYS Technologies limited.


    Mitsubishi Regional Jet(Mitsubishi Aircraft Corporation)



    ·         Concept of design criteria.

    ·         Model Based Definition (MBD) activities for frames,Stringers,Splice for fuselage.

    ·         Creating Reference Documents for the Evidence reports.

    ·         Model Based Definition activities.

    §  KELTRON

    (A Govt Undertaking)

    (June 2010 - Feb 2012)

    Indian Space Research Organisation,

    ISRO Satellite Centre.



    ·         AIT, Assembly Integration and Testing sequence procedure and documentationfor Scientific Remote Sensing Satellites.

    ·         Expert in Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS) & Expert in Routing by using CATIA V5 Electrical Harness Design.

    ·        Validating the harness tests, manufacturing.

    ·         Design and realization of Electrical Distribution System (EDS).

    ·         Clean Room Functional and Integration test (FIT) for all subsystem.

    §  Classic Industries

    (June 2009-May 2010)


    §  Bharat Heavy Electricals limited (BHEL)

    ·         Designing the job material as per BHEL requirement by using 2D - AUTOCAD.

    ·         Quality checks done as per QA documents.

    ·         Fabricating and testing the manufactured job materials.

    • Interact with customer for seeking clarifications, resolving technical issues, for acceptance of deliverable.


    Tool Experience

    §  CATIA V5

     2 Years

    Electrical Harness Design

    §  CATIA V5

     4 Months

    Functional Tolerance and Annotation (FTA)


    Educational Qualification


    Branch / Discipline

    Institute, University

    % &Year

    Bachelor of Engineering (BE)

    Electrical and Electronics Engineering

    K.S.Rangasamy College of Technology,

    Anna University-Chennai

    75.13 &


    First Class distinction

    Higher Secondary

    State Board, Tamilnadu

    Bishop Heber Higher Secondary School

    71.83% & First Class /2005


    State Board, Tamilnadu

    K.A.P.V Higher Secondary School

    81.6% & First Class /2003



    §  CATIA V5 (Electrical)

    20 Days

    EDS Technologies(Certified Education Partner to Dassault Systemes, France)

    §  CATIAV5

    30 Days

    Infosys (Internal Training)


    §  AUTOCAD

    30 Days

    Practical Technologies, AUTODESK Certified





    Project #1

    PSLV C-16


    YOUTHSAT(Indo –Russian Mission)


    ISRO Satellite Centre


    Jun 2010 to April 2011 (11  Months)

    Tool /s

    CATIA V5

    Work Location

    Indian Space Research Organisation, Bangalore


    Integration Engineer


    A cooperative joint scientific mission between India and Russia (Moscow University).The micro satellite bus is planned and designed to carry different kinds of payloads like earth imaging, atmospheric applications, weather monitoring, stellar observations, scientific experiments etc.




























    Harness Design, Fabrication, Testing and Routing:

    ·         Generation of Electrical Integration requirements such as Harness path, inserts, cutouts etc., as per EMI/EMC aspects.

    ·         Good knowledge of CATIA V5 Electrical Harness Discipline.

    ·         Expert in Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS).

    ·         Responsible for Data base management, which includes Harness design, Compilation of data cards and matching, patch allocation, generation of worksheets as per subsystem requirements.

    ·         Electrical Interface Definition includes functional description, signal characteristics, originating connectors details, destination connectors details, types of wire used etc. responsible for matching of source to destination subsystem by using PC based software.

    ·         Involved in Electromagnetic compatibility (EMC) design and Electro-Static Discharge (ESD).

    ·         Development of a database for satellite and definitions for electrical wiring.

    • Involved in implementation of Grounding scheme and ESD control measure.
    • Involved in bracket design and finalizing the location for patch connectors.

    ·         Designed Mil-std-1553B-Busharness layout to minimize Bus breaks tested and installed.


    CLEANROOM Level Assembly Integration and testing(AIT):

    • Functional and Integration test (FIT) procedure for all subsystem in spacecraft were prepared.
    • Testing of all subsystems on spacecraft such as On Board Computer(OBC), Inertial Reference Unit(IRU), Power Systems, Sensors, Magnetic Torquer, Solid State Recorder(SSR), Base Data Handling Systems(BDH), RF Systems, Thermal Elements, Reaction Control System(RCS)  and payload systems.
    • Monitoring and analysis of satellite telemetry data.
    • Tele Command of satellites for all required operations.
    • Providing support to and cooperate with other teams for the day to day operations of the satellites.

    Dis-assembled Integrated Satellite Testing

    During this phase all subassemblies are interconnected using test cables.

    ·         Umbilical Checks, Interconnection Checks

    ·         Isolation Checks, Functional Checks

    ·         Tele command Checks, Telemetry Checks

    ·         Electrical ground support equipment(EGSE)

    ·         Panel Closure Activity

    Assembled Integrated Satellite Testing (IST)

    • For all subsystem and payload checks will be done.

    ·         Solar panel deployment Test, Illumination Test

    ·         Antenna Deployment Test

    ·         Thermo vacuum Test, Vibration Test

    • Supported in integration of RUSSIAN Moscow university payload SolRad.

    ·         Supported in testing of Youthsat spacecraft with PSLV C-16 in Shriharikota



    Project #2



    SARAL (Indo –France CNES Mission)


    ISRO Satellite Centre


    Dec 2011 to Feb 2012 ( 15 Months)

    Tool /s

    CATIA V5

    Work Location

    Indian Space Research Organisation, Bangalore



    Integration Engineer


    SARAL is a joint scientific mission between India and France (CNES). The first mission with these payloads is called 'SARAL' (Satellite for ARGOS and ALTIKA Payloads) mission.



    ·         Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS).Responsible for Data base management.

    ·         Development of a database for satellite and definitions for electrical wiring.

    • Check and Approve the CATIA Models and Drawings like positioning, face etc., as per requirements.

    ·         Finalizing the harness routing and anchoring point for the spacecraft based on the electrical interfaces of all subsystems.


    Project #3

    Fuselage Designing for Aircraft


    Mitsubishi Regional Jet 70-90 seating


    Mitsubishi Aircraft Corporation (MAC),Japan


    July 2012 to Till date (4 Months)

    Tool /s

    CATIA V5

    Work Location

    Infosys Technologies Limited


    Design Engineer, Aircraft fuselage


    The Mitsubishi Regional Jet (MRJ) is a passenger jet aircraft seating 70–90 passengers manufactured by Mitsubishi. The airliner has been produced in three Fuselage lengths. The Fuselage is a pressurized Semi-Monocoque structure formed from circumferential frames, longitudinal stringers and skin.


    ·         Involved in MBD (Model Based Definition) activity of Frames (Both Sheet metal, Machined Frames), Stringers, Stringer clips, Stringer splice.

    ·         Creating Reference documents, Capture documentand Evidence reports.

    ·         Creating MBD models for the parts at DDM, IDM & ADM Stages.

    ·         Model based definition (MBD) creation using FTA (GD&T) module for different aircraft components

    ·         Installation Definition Model, creation using shape design & FTA in CATIA V5


    Personal Details


    Date of Birth

    December -02- 1987



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