Attention is given to a space-borne engine plume experiment study to fly an experiment which will both verify and quantify the reduced contamination from advanced rhenium-iridium earth-storable bipropellant rockets (hot rockets) and provide a correlation between high-fidelity, in-space measurements and theoretical plume and surface contamination models. The experiment conceptual design is based on survey results from plume and contamination technologists throughout the U.S. With respect to shuttle use, cursory investigations validate Hitchhiker availability and adaptability, adequate remote manipulator system (RMS) articulation and dynamic capability, acceptable RMS attachment capability, adequate power and telemetry capability, and adequate flight altitude and attitude/orbital capability.


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    Title :

    Hot rocket plume experiment - Survey and conceptual design


    Contributors:

    Conference:

    Optical System Contamination: Effects, Measurement, Control III ; 1992 ; San Diego,CA,United States


    Published in:

    Publication date :

    1992-12-18





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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