The propulsion system is a critical aspect of the performance and feasibility of a Mars aircraft. Propulsion system mass and performance greatly influence the aircraft s design and mission capabilities. Various propulsion systems were analyzed to estimate the system mass necessary for producing 35N of thrust within the Mars environment. Three main categories of propulsion systems were considered: electric systems, combustion engine systems and rocket systems. Also, the system masses were compared for mission durations of 1, 2, and 4 h.


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    Title :

    Comparison of Mars Aircraft Propulsion Systems


    Contributors:

    Publication date :

    2003-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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