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  • 1
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2014-09-17
    Description: Forces on tethered satellites, tether tension as a function of the effective mass, and parameters of candidate tether materials are examined. Illustrations show: stabilization control law; tethered satellite deployment and retrieval; angular momentum; electric motor effect reboost; a very long tether phenomenon; shuttle tethered satellite effects on the orbiter; artificial gravity; tethered satellite rendezvous docking relative velocity; and scaling up from the shuttle/TSS. Limitations of the tethered satellite system and of tether properties as well as cost/benefits trades for future applications are considered.
    Keywords: MECHANICAL ENGINEERING
    Type: Appl. of Tethers in Space, Vol. 1; 15 p
    Format: text
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