HERMeS - Hall Effect Rocket with Magnetic Shielding. Developed through a joint effort by NASA/GRC and the Jet Propulsion Laboratory (JPL). Design goals: High power (12.5 kW) high Isp (3000 sec), high efficiency (> 60%), high throughput (10,000 kg), reduced plasma erosion and increased life (5 yrs) to support Asteroid Redirect Robotic Mission (ARRM). Further details see "Performance, Facility Pressure Effects and Stability Characterization Tests of NASAs HERMeS Thruster" by H. Kamhawi and team. Hall Thrusters (HT) inherently operate at elevated temperatures approx. 600 C (or more). Due to electric magnetic (E x B) fields used to ionize and accelerate propellant gas particles (i.e., plasma). Cooling is largely limited to radiation in vacuum environment.Thus the hardware components must withstand large start-up delta-T's. HT's are constructed of multiple materials; assorted metals, non-metals and ceramics for their required electrical and magnetic properties. To mitigate thermal stresses HT design must accommodate the differential thermal growth from a wide range of material Coef. of Thermal Expansion (CTEs). Prohibiting the use of some bolted/torqued interfaces.Commonly use spring loaded interfaces, particularly at the metal-to-ceramic interfaces to allow for slippage.However most component interfaces must also effectively conduct heat to the external surfaces for dissipation by radiation.Thus contact pressure and area are important.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hall Thruster Thermal Modeling and Test Data Correlation


    Beteiligte:
    Myers, James (Autor:in)

    Kongress:

    AIAA Joint Propulsion Conference ; 2016 ; Salt Lake City, UT, United States


    Erscheinungsdatum :

    2016-07-25


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hall Thruster Thermal Modeling and Test Data Correlation

    Myers, James / Kamhawi, Hani / Yim, John et al. | NTRS | 2016


    Hall Thruster Thermal Modeling and Test Data Correlation

    Myers, James L. / Kamhawi, Hani / Yim, John et al. | AIAA | 2016


    HALL THRUSTER THERMAL MODELING AND TEST DATA CORRELATION (AIAA 2016-4535)

    Myers, James L. / Kamhawi, Hani / Yim, John et al. | British Library Conference Proceedings | 2016


    Modeling the Hall thruster

    Fruchtman, A. / Fisch, N. | AIAA | 1998


    HALL THRUSTER

    JORNS BENJAMIN / HURLEY WILLIAM / MARKS THOMAS et al. | Europäisches Patentamt | 2023

    Freier Zugriff