The degradation of the pulsed performance of low-thrust, cold-gas, jet reaction systems is shown; also, the experimental data are compared with analytical results. Preliminary experimental results using anhydrous ammonia gas as a propellant are included. The experimentation conducted on a single-axis attitude control system utilizing a fluid flywheel is presented, along with an analysis of this system. The preliminary results of an analysis of the singleaxis vehicle simulator incremental follow-up servo are given. In addition, a specific impulse pneumatic test facility and a manned tracking target symbol generator are described. (Author)


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    Title :

    Electonics Research Program. Satellite Attitude Control System Experiments


    Contributors:
    D. J. Griep (author)

    Publication date :

    1964


    Size :

    84 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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