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  • HiTOS: A High-Temperature Optical Fiber-based sensor system for Space structures

    Paper number

    IAC-12,D1,2,9,x14647

    Author

    Mr. Francisco García-de-Quirós, EMXYS (Embedded Instruments and Systems S.L), Spain

    Coauthor

    Dr. Jose Antonio Carrasco, EMXYS (Embedded Instruments and Systems S.L), Spain

    Coauthor

    Dr. Iain McKenzie, ESA european space agency, The Netherlands

    Coauthor

    Dr. Salvador Sales, Universidad Politécnica de Valencia, Spain

    Coauthor

    Mr. David Barrera, Universidad Politécnica de Valencia, Spain

    Coauthor

    Dr. Joel Villatoro, ICFO-Institute of Photonic Sciences, Spain

    Coauthor

    Dr. Vittoria Finazzi, ICFO-Institute of Photonic Sciences, Spain

    Coauthor

    Mr. Jesus Marcos, INASMET-TECNALIA, Spain

    Coauthor

    Dr. María Parco, TECNALIA, Spain

    Coauthor

    Dr. Valerio Pruneri, ICFO-Institute of Photonic Sciences, Spain

    Year

    2012

    Abstract
    Temperature and strain sensors based in optical fiber, such as Fiber Bragg Gratings (FBG), present important advantages over the traditional technologies, like thermocouples, in terms of mass/weight, EMI immunity, chemical compatibility, multiplexing capabilities, (i.e. simplification of harness), etc.
    
    Nevertheless, standard FBG technology is intrinsically not suitable for temperature ranges above 500ºC,  which limits its use on high-temperature applications like Thermal Protection Systems (TPS) or propulsion elements.
    
    The HiTOS project consists in the development of a High-Temperature (>1000ºC) sensor system based on a new generation of Bragg gratings called regenerative Bragg Gratings (rFBG). This manufacturing technique enables the FBG technology to a higher range of operation temperatures, opening an entirely new scope of applications in Space Vehicles.
    
    In this contribution, the HiTOS project is described as well as its main results and conclusions, obtained after the final characterization tests  performed over the prototype implemented, which included all the elements of a future Space qualified version of the sensor system.
    Abstract document

    IAC-12,D1,2,9,x14647.brief.pdf

    Manuscript document

    IAC-12,D1,2,9,x14647.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.