The successful performance of the five individual demonstrations of MARS IN-SITU-PROPELLANT-PRODUCTION PRECURSOR (MIP) will provide both knowledge of and confidence in the reliability of this technology. At the completion of this flight demonstration, the MIP Team will be able to: (a) recommend preferred hardware configurations for the intake and adsorption of carbon dioxide from the Martian atmosphere; (b) understand the performance characteristics of zirconia cells to generate propellant-grade oxygen; (c) understand long-term performance characteristics of advanced solar cells/arrays operated in the actual Mars environment; (d) evaluate the functionality of methods to mitigate the deposition of airborne dust onto solar arrays; and (e) recommend preferred hardware designs for innovative thermal management including the radiation of heat to the outside environment.


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    Titel :

    2001 Mars In-Situ-Propellant-Production Precursor (MIP) Flight Demonstration


    Beteiligte:
    D. I. Kaplan (Autor:in) / R. S. Baird (Autor:in) / J. E. Ratliff (Autor:in) / C. R. Baraona (Autor:in) / P. P. Jenkins (Autor:in)

    Erscheinungsdatum :

    2000


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The 2001 Mars In-Situ-Propellant-Production Precursor (MIP) Flight Demonstration

    Kaplan, David I. / Baird, R. Scott / Ratliff, James E. et al. | NTRS | 2000


    The Mars In-Situ-Propellant-Production Precursor (MIP) Flight Demonstration

    Kaplan, D. I. / Ratliff, J. E. / Baird, R. S. et al. | NTRS | 1999


    Mars In-Situ Propellant Production Precursor (MIP) Flight Demonstration Project: Overview

    Kaplan, D. I. / Ratliff, J. E. / Baird, R. S. et al. | NTRS | 1999


    Mars In-Situ Propellant Production Precursor (MIP) Flight Demonstration Project: Overview

    Kaplan, D. I. / Ratliff, J. E. / Sanders, G. B. et al. | NTRS | 1999