This paper describes a simulation designed to evaluate a communications link between the Earth and the Mars Pathfinder Lander module as it descends under a parachute through the Martian atmosphere toward the planet's surface. The link includes a transmitter and a low gain antenna on the spacecraft and a receiving antenna and receiver on the Earth as well as a simulation of the dynamics of the spacecraft.


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    Titel :

    An Application fo the Virtual Spacecraft Concept in Evaluation of the Mars Pathfinder Lander Low Gain Antenna


    Beteiligte:
    Pogorelski, R. J. (Autor:in) / Beckon, R. J. (Autor:in)

    Erscheinungsdatum :

    1997-07-13


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch