The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) will test Hyper-sonic Inflatable Aerodynamic Decelerator (HIAD) technology. Temperature measurements are taken across the vehicle to address a Level 1 mission requirement regarding performance of the Flexible Thermal Protection System (F-TPS). Temperature measurements are made using dozens of thermocouples (TCs) embedded within the F-TPS at different depths and various locations shown in Figure 1.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Electrical Shorting of Thermocouples in Atmospheric Entry Applications


    Beteiligte:
    Cole D Kazemba (Autor:in) / J D Williams (Autor:in) / R A Miller (Autor:in) / G T Swanson (Autor:in) / S J Hughes (Autor:in)

    Kongress:

    17th International Planetary Probe Workshop (IPPW 2020) ; 2020 ; Monterey, CA, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Electrical Shorting of Thermocouples in Flexible Thermal Protection System Materials

    Miller, Ruth A. / Kazemba, Cole D. / Swanson, Gregory T. et al. | AIAA | 2023


    4300° F thermocouples for re-entry vehicle applications -- 1

    Bolling, N.F. | Engineering Index Backfile | 1963


    4300 F Thermocouples for Re-Entry Vehicle Applications Part II

    Pustell, Robert A. | SAE Technical Papers | 1963



    Armament Shorting Arrangement

    W. B. Whittaker | NTIS | 1981