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  • SPACE VEHICLES  (1)
  • 1970-1974  (1)
  • 1930-1934
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  • 1970-1974  (1)
  • 1930-1934
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    Publication Date: 2019-06-27
    Description: The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes. This coupling results in interaction between the pogo and control systems. A detailed model of representative space shuttle structure, feedline, control, and engine systems revealed the coupled system may be unstable even though the pogo and control systems are stable individually. A method is developed for predicting the coupled system stability in terms of the stability of the separate systems.
    Keywords: SPACE VEHICLES
    Type: NASA-CR-2154 , MDC-G2961
    Format: application/pdf
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