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Displacement simulation for spacecraft structure

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

The paper presents a technique of forming and evaluating the allowable clearance between a launch vehicle fairing and spacecraft.

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Authors and Affiliations

  1. Reshetnev Siberian State Aerospace University, pr. imeni gazety “Krasnoyarskii rabochii” 31, Krasnoyarsk, Russia

    S. N. Senashov

  2. Reshetnev AO ISS, ul. Lenina 52, Zheleznogorsk, Krasnoyarskii krai, 662972, Russia

    D. F. Balyakov

Authors
  1. S. N. Senashov
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  2. D. F. Balyakov
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Corresponding author

Correspondence to D. F. Balyakov.

Additional information

Original Russian Text © S.I. Senashov, D.F. Balyakov, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 1, pp. 55–60.

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Senashov, S.N., Balyakov, D.F. Displacement simulation for spacecraft structure. Russ. Aeronaut. 60, 57–63 (2017). https://doi.org/10.3103/S1068799817010093

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  • DOI: https://doi.org/10.3103/S1068799817010093

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