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Analytical Estimates of the Fairing Flaps Separation Dynamics of the Rocket and Space Systems

  • STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES
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Abstract

The paper proposes an approach to study the influence of the flaps spatial movement as a solid body and the elastic relative vibrations of their structure on the flaps separation process safety, which means the guaranteed exclusion of their collisions with both the launch vehicle and the payload. A number of relevant analytical estimates for calculating the spatial relative motion and the level of flaps vibrations during their separation process is obtained.

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ACKNOWLEDGEMENTS

The work was carried out within the framework of the state task; the number of the state registration of the topic is AAAA-A19-119012290177-0.

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Authors and Affiliations

  1. Institute of Applied Mechanics, Russian Academy of Sciences, pr. Leningradskii 7, 125040, Moscow, Russia

    V. N. Bakulin

  2. PAO S.P. Korolev Rocket and Space Corporation Energiya, ul. Lenina 4A, 141070, Korolev, Moscow oblast, Russia

    S. V. Borzykh & K. V. Tereshina

Authors
  1. V. N. Bakulin
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  2. S. V. Borzykh
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  3. K. V. Tereshina
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Corresponding author

Correspondence to V. N. Bakulin.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 14 - 21.

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Bakulin, V.N., Borzykh, S.V. & Tereshina, K.V. Analytical Estimates of the Fairing Flaps Separation Dynamics of the Rocket and Space Systems. Russ. Aeronaut. 64, 376–384 (2021). https://doi.org/10.3103/S1068799821030028

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  • DOI: https://doi.org/10.3103/S1068799821030028

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