A high-fidelity simulation of a conceptual Mars Ascent Vehicle has been developed for end-to-end performance evaluation. The simulation environment is the Dynamics Simulator for Entry, Descent and Surface landing (DSENDS). The simulation work includes the modeling of the multi-body components, Martian environment, flight software and mission timeline. Using this simulation environment, the end-to-end MAV flight performance is evaluated, both in the nominal scenario and in perturbed off-nominal scenarios where model uncertainties are taken into account.


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    Title :

    Hybrid propulsion Mars Ascent Vehicle concept flight performance analysis


    Contributors:


    Publication date :

    2017-03-01


    Size :

    1341124 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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