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Method of Taking into Account Influence of Thermal Shock on Dynamics of Small Satellite and its Use in Analysis of Microaccelerations

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Abstract

The article resents a method that allows taking into account the effect of thermal shock on the satellite dynamics. This method make possible to correct the motion model of a small satellite by adding effect of thermal shock to the model. Numerical modeling was carried out to analyze microaccelerations from thermal shock in the a one-dimensional model of thermal conductivity. The results of the research can be used to create small satellite for technological purposes.

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Funding

This study was supported by the Russian Science Foundation (Project No. 22–19-00160).

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Authors and Affiliations

  1. Samara National Research University, Samara, Russia

    Andry Sedelnikov, Valeria Serdakova & Alexandra Nikolaeva

Authors
  1. Andry Sedelnikov
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  2. Valeria Serdakova
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  3. Alexandra Nikolaeva
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Contributions

A.V. Sedelnikov developed the concept of the work, conducted the derivation of the equations of the model, wrote the text of the work. V.V. Serdakova wrote the introduction, conducted a literature review. A.S. Nikolaeva performed numerical modeling environment and verification of modeling results. All authors reviewed the manuscript.

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Correspondence to Andry Sedelnikov.

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Sedelnikov, A., Serdakova, V. & Nikolaeva, A. Method of Taking into Account Influence of Thermal Shock on Dynamics of Small Satellite and its Use in Analysis of Microaccelerations. Microgravity Sci. Technol. 35, 25 (2023). https://doi.org/10.1007/s12217-023-10049-w

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