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    Minimizing spacecraft structure control-system interaction. (1969)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: Spacecraft design for minimization of structure interaction with control system, noting susceptibility of extendible booms to solar environment
    Keywords: SPACE VEHICLES
    Type: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, STRUCTURAL DYNAMICS AND AEROELASTICITY SPECIALIST CONFERENCE; APRIL 16, 17, 1969; NEW ORLEANS, LA.
    Format: text
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