This paper describes a high fidelity mission concept systems testbed at JPL that was used to support the InSight (Interior Exploration Using Seismic Investigations, Geodesy, and Heat Transport) mission concept study. The InSight mission would conduct geophysical exploration of Mars' interior using three instruments 1. SEIS seismometer monitors seismic activity and tidal displacements; 2. RISE X-band radio Doppler tracking experiment measures rotational variations; and 3. HP3: Heat-flow and Physical Properties Probe determines the geothermal heat flux. CNES contributes SEIS and DLR contributes HP3. The measurements from these instruments would yield information about processes that occurred during the initial accretion of the planet, the formation and differentiation of its core, crust, and mantle, and subsequent evolution of its interior. The SEIS and HP3 instruments will be deployed to the surface of Mars using a robotic arm similar to the robotic arm used on the Mars Phoenix Lander mission and operational experience inherited from Phoenix and MER. The SEIS and HP3 will be monitored every three hours for one Mars year, with no ground-in-the-loop interaction required. InSight was one of three proposed missions selected by NASA Discovery Program in May 2011 for funding to conduct preliminary design studies and analyses. InSight was selected in August 2012 as the 12th mission in the NASA Discovery Program.


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    Titel :

    Instrument deployment testbed: For planetary surface geophysical exploration


    Beteiligte:
    Trebi-Ollennu, Ashitey (Autor:in) / Rankin, Arturo L. (Autor:in) / Cheng, Yang (Autor:in) / Tso, Kam S (Autor:in) / Deen, Robert G (Autor:in) / Aghazarian, Hrand (Autor:in) / Kulczycki, Eric A. (Autor:in) / Bonitz, Robert G (Autor:in) / Alkalai, Leon (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2013-03-01


    Format / Umfang :

    4183749 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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