Teleoperator Maneuvering System (TMS) versus integral spacecraft propulsion, spacecraft maintenance, cost benefits, launch prices, integral propulsion length penalties, remote maintenance versus EVA, potential weight reduction benefits, basing mode, mission models and payload requirements, and program profitability are discussed.


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    Title :

    Teleoperator Maneuvering System (TMS) Benefits Assessment Study. Volume 1: Executive Summary


    Publication date :

    1983


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English