Results for trajectory analysis, fuel analysis, and analysis of aerobraking maneuvers are presented. Calculations are included for thickness and mass of the propellant tanks; determination of weight (avionics module); numerical integration program; hydrostatic pressure due to acceleration; and propellant tank pressurization.


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    Title :

    Unmanned, Space-Based, Reusable Orbital Transfer Vehicle, Darves. Volume 2. Data and Calculations


    Publication date :

    1988


    Size :

    37 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English