For several proposed configurations of the modular space station, the gravity gradient torque distribution is examined for both Y-POP and inertial hold orbits. The necessary equations are derived to allow for solar panel gimbaling, and a procedure is established which will allow any desired space station configuration to be built up. Results indicated that solar panel gimbaling can be a significant factor in the torque distribution in Y-POP orbits. In addition, for the two configurations that were plotted, bias torque magnitudes varied widely in inertial hold modes. (Author)


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    Title :

    Gravity Gradient Torque Profiles over an Orbit for Arbitrary Modular Space Station Configurations in the Y-Pop and Inertial Hold Modes


    Contributors:

    Publication date :

    1972


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English