The temperatures produced by the various components in the propulsion system of rockets and missiles determine the performance of the rocket. Since these temperatures occur very rapidly and under extreme conditions, standard thermocouples fail before any meaningful temperatures are measured. This paper describes the features of a special family of high performance thermocouples, which can measure these transient temperatures with millisecond response times and under the most severe conditions of erosion. Examples of igniter, propellant and rocket nozzle temperatures are included in this paper. Also included is heat flux measurements made by these sensors in rocket applications.


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    Titel :

    Unique thermocouple to measure the temperatures of squibs, igniters, propellants, and rocket nozzles


    Beteiligte:

    Kongress:

    Sensors for Propulsion Measurement Applications ; 2006 ; Orlando (Kissimmee),Florida,United States


    Erschienen in:

    Erscheinungsdatum :

    10.05.2006





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Unique thermocouple to measure the temperatures of squibs, igniters, propellants, and rocket nozzles [6222-03]

    Nanigian, J. / Nanigian, D. / SPIE-- the International Society for Optical Engineering | British Library Conference Proceedings | 2006



    Uncooled Rocket Nozzles for Ultra-High Temperature Propellants

    Kraus, George | SAE Technical Papers | 1962


    RECOMBINATION LOSSES IN ROCKET NOZZLES WITH STORABLE PROPELLANTS

    KOPPANG, R. R. / SIMKIN, D. J. | AIAA | 1963


    CuO/Al Igniters For Solid Rocket Motor Ignition

    Reese, David / Wright, Darren / Son, Steven | AIAA | 2011