A fiber-optic temperature sensor has been developed for aerospace applications on the basis of the time rate of decay (TRD) principle, with a view to an operational temperature range of -60 to 350 C. This TRD system has completed qualification testing and will then undergo flight tests. Attention is presently given to the design and performance of four low temperature sensors that are subelements of the larger sensor system; in order to convert analog signals into over/under temperature indications, simple comparators are implemented in software.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fiber optic temperature sensor for aerospace applications


    Beteiligte:

    Kongress:

    Fiber Optic Systems for Mobile Platforms IV ; 1991 ; San Jose,CA,United States


    Erschienen in:

    Erscheinungsdatum :

    1991-02-01





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Fiber-Optic Sensor Systems For Aerospace Applications

    Udd, E. / Michal, R. J. / Higley, S . E. et al. | SPIE | 1988



    A fiber-optic current sensor for aerospace applications

    Patterson, R.L. / Rose, A.H. / Tang, D. et al. | Tema Archiv | 1990


    A fiber-optic current sensor for aerospace applications

    Patterson, Richard L. / Rose, A. H. / Tang, D. et al. | NTRS | 1990