Skip to main content
SpringerLink
Log in

Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity

  • Original Article
  • Published:
Microgravity Science and Technology Aims and scope Submit manuscript

Abstract

The article considers the thermal shock of large elastic elements of a spacecraft leaving the Earth's shadow. The stress–strain state of the element is analyzed to estimate additional microaccelerations from a thermal shock. Beside the most dangerous cases, the possible initial deflection of the elastic element at the time of the thermal shock is also considered. This deflection can be related to the natural vibrations of elastic elements. The obtained results demonstrate a significant decrease in additional microaccelerations from a thermal shock at certain values of the initial deflection. It was also found that an elastic element can lose stability when bending stresses are added to thermal stresses. The results of the investigation can be used in the design and usage of small technological spacecraft.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Subscribe and save

Springer+ Basic
$34.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or eBook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7

Similar content being viewed by others

References

  • Anshakov, G.P., Belousov, A.I., Sedelnikov, A.V., et al.: Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion. Russian Aeronautics 61(3), 347–354 (2018)

    Article  Google Scholar 

  • Belousov, A.I., Sedelnikov, A.V.: Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory. Russian Aeronautics 56(3), 60–63 (2013)

    Article  Google Scholar 

  • Belousova, D.A., Serdakova, V.V.: Modeling the temperature shock of elastic elements using a one-dimensional model of thermal conductivity. Int J of Modeling, Simulation, and Sci Computing. 11(6), 2050060 (2020)

  • Gorozhankina, A.S., Orlov, D.I., Belousova, D.A.: Problems of development motion control algorithms for a small spacecraft for technological purpose taking into account temperature deformations of solar panels. J. Conf. Ser. 1546, 012015 (2020) 

  • Ivanov, D.S., Meus, S.V., Ovchinnikov, A.V., et al.: Methods for the vibration determination and parameter identification of spacecraft with flexible structures, Journal of Computer and System Science. International 56, 311–327 (2017)

    MATH  Google Scholar 

  • Li, Q., Liu, L., Yang, H.: High accuracy and multi-target acquisition, pointing and tracking under satellite micro-vibrations. Microgravity Sci. Technol. 32(4), 715–727 (2020)

    Article  Google Scholar 

  • Lyubimova, T., Zubova, N., Shevtsova, V.: Effects of Non-Uniform Temperature of the Walls on the Soret Experiment. Microgravity Sci. Technol. 31(1), 1–11 (2019)

    Article  Google Scholar 

  • Manu O., Verna J.K., Karla P., et al.: Performance analysis of effect of vibrations on solar panel conversion efficiency, International conference on smart technology for smart nation, 635–638 (2017)

  • Oda M., Hagiwara Yu., Suzuki S., et al.: Measurement of satellite solar array panel vibrations caused by tnermal snap and gas jet thruster firing, in: Resent advances in vibrations analysis, Chapter 7, 123–140 (2011)

  • Perminov, A.V., Lyubimova, T.P., Nikulina, S.A.: Influence of High Frequency Vertical Vibrations on Convective Regimes in a Closed Cavity at Normal and Low Gravity Conditions. Microgravity Sci. Tech. 33, 55 (2021)

  • Sedelnikov, A.V.: Fractal quality of microaccelerations. Microgravity Sci. Technol. 24(5), 345–350 (2012)

    Article  Google Scholar 

  • Sedelnikov, A.V., Orlov, D.I.: Development of control algorithms for the orbital motion of a small technological spacecraft with a shadow portion of the orbit. Microgravity Sci. Technol. 32(5), 941–951 (2020)

    Article  Google Scholar 

  • Sedelnikov, A.V., Orlov, D.I.: Analysis of the significance of the influence of various components of the disturbance from a temperature shock on the level of microaccelerations in the internal environment of a small spacecraft. Microgravity Sci. Tech. 33(2), 22 (2021)

  • Sedelnikov, A.V.: Algorithm for restoring information of current from solar panels of a small spacecraft prototype “Aist” with help of normality conditions. Journal of Aeronautics, Astronautics, and Aviation 54(1), 67–76 (2022)

    Google Scholar 

  • Sedelnikov, A.V., Serpukhova, A.A.: Simulation of a flexible spacecraft motion to evaluate microaccelerations. Russian Aeronautics 52(4), 484–497 (2009)

    Article  Google Scholar 

  • Sedelnikov, A.V., Serdakova, V.V., Khnyreva, E.S.: Construction of the criterion for using a two-dimensional thermal conductivity model to describe the stress-strain state of a thin plate under the thermal shock. Microgravity Sci. Tech. 33(6), 65 (2021)

  • Sharifulin, V.A., Lyubimova, T.P.: A Hysteresis of Supercritical Water Convection in an Open Elongated Cavity at a Fixed Vertical Heat Flux. Microgravity Sci. Technol. 33, 38 (2021)

    Article  Google Scholar 

  • Shen, Z., Hu, G.: Thermally Induced Dynamics of a Spinning Spacecraft with an Axial Flexible Boom. J. Spacecr. Rocket. 52(5), 1503–1508 (2015)

    Article  Google Scholar 

  • Shen, Z., Tian, Q., Liu, X., Hu, G.: Thermally induced vibrations of flexible beams using Absolute Nodal Coordinate Formulation. Aerosp. Sci. Technol. 29, 386–393 (2013)

    Article  Google Scholar 

  • Shevtsova, V.: Investigation of diffusive and optical properties of vapour-air mixtures: The benefits of interferometry, Elsevier Ltd. (2021)

  • Shevchenko, V., Mialdun, A., Yasnou, V., Y. Lyulin, V., Ouerdane, H., Shevtsova, V.: Investigation of diffusive and optical properties of vapour-air mixtures: The benefits of interferometry”. Chem. Eng. Sci. 233, 116433 (2021)

  • Taneeva, A.S.: The formation of the target function in the design of a small spacecraft for technological purposes. J. Phys. Conf. Ser. 1901(1), 012026 (2021)

Download references

Acknowledgements

The work was carried out within the framework of the project "Development of scientific and technical foundations and design solutions that ensure the implementation of the required level of microaccelerations on board small spacecraft" (No. 22-19-00483).

Author information

Authors and Affiliations

  1. Samara National Research University, Samara, Russia

    Sedelnikov A.V., Glushkov S.V., Nikolaeva A.S. & Evtushenko M.A.

  2. Amur State University, Blagoveshchensk, Russia

    Serdakova V.V.

Authors
  1. Sedelnikov A.V.
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Serdakova V.V.
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Glushkov S.V.
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Nikolaeva A.S.
    View author publications

    You can also search for this author in PubMed Google Scholar

  5. Evtushenko M.A.
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Sedelnikov A.V..

Ethics declarations

Conflict of interest

The authors declare that they have no conflict of interest.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

A.V., S., V.V., S., S.V., G. et al. Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity. Microgravity Sci. Technol. 34, 22 (2022). https://doi.org/10.1007/s12217-022-09938-3

Download citation

  • Received:

  • Accepted:

  • Published:

  • DOI: https://doi.org/10.1007/s12217-022-09938-3

Keywords

Search

Navigation