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A Study of the Dynamic Characteristics of the Cyclone-4 Launch Vehicle on the Basis of a Continuum Rod Model

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A technology for the creation of dynamic simulation models of liquid-propellant launch vehicles on the basis of a combined continuum rod scheme is considered. The procedure has been successfully implemented and evaluated for the Cyclone-4 launch vehicle as an example. Amplitude-frequency characteristics of the launch vehicle in different flight segments have been determined, and the obtained results have been analyzed.

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References

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Authors and Affiliations

  1. National Technical University of Ukraine “Kiev Polytechnic Institute,”, Kiev, Ukraine

    A. S. Konyukhov, A. S. Tsybenko & A. A. Rybalka

Authors
  1. A. S. Konyukhov
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  2. A. S. Tsybenko
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  3. A. A. Rybalka
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Translated from Problemy Prochnosti, No. 4, pp. 26 – 30, July – August, 2015.

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Konyukhov, A.S., Tsybenko, A.S. & Rybalka, A.A. A Study of the Dynamic Characteristics of the Cyclone-4 Launch Vehicle on the Basis of a Continuum Rod Model. Strength Mater 47, 532–535 (2015). https://doi.org/10.1007/s11223-015-9686-3

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  • DOI: https://doi.org/10.1007/s11223-015-9686-3

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