This viewgraph presentation reviews the drop test used to test the Mars lander. The objective of the test was to demonstrate the structural and functional integrity of the development test Model (DTM). Rover Basepetal when subjected to the landing event. The test module was instrumented with accelerometers to measure the kinematic response of the test article during impact.


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    Titel :

    Qualifying Spirit and Opportunity to Martian Landing Loads with Centrifuge Testing


    Beteiligte:

    Kongress:

    Spacecraft and Launch Vehicle Dynamic Environments Workshop ; 2004 ; El Segundo, CA, United States


    Erscheinungsdatum :

    2004-06-22


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Landing Loads

    Lomax, Ted L. | AIAA | 1996


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    Sagan, C. / Swan, P. R. | NTRS | 1965


    Martian landing sites for the voyager mission

    SAGAN, C. / HARVARD U. / CAMBRIDGE et al. | AIAA | 1965


    Geology of six possible Martian landing sites

    Masursky, Harold / Dial, A. L., Jr. / Strobell, M. E. et al. | NTRS | 1987