Abstract
The paper analyzes the influence of various disturbing components arising from a temperature shock of large elastic elements of a small spacecraft structure on the level of microaccelerations of the internal environment. The stability loss of a flat equilibrium shape of an elastic element of a small spacecraft is considered, as well as its all-round expansion when it moves from the shadow area to the illuminated part of the orbit. Conclusions are drawn about the significance of the influence of various factors in modeling the microacceleration field. The results obtained can be used in the design of small technological spacecraft.
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References
Belousova, D.A., Serdakova, V.V.: Modeling the temperature shock of elastic elements using a one-dimensional model of thermal conductivity. Int. J. Model Simul. Sci. Comput. 11(6), 2050060 (2020)
Bisht, K.S., Dreyer, M.E.: Phase separation in porous media integrated capillary channels. Microgravity Sci. Technol. 32(6), 1001–1018 (2020)
Gaponenko, Y., Gousselnikov, V., Santos, C.I.A.V., Shevtsova, V.: Near-critical behavior of Fick diffusion coefficient in Taylor dispersion experiments. Microgravity Sci. Technol. 31(5), 475–486 (2019)
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. Phys. Conf. Ser. 1546, 012015 (2020)
Lipovtsev, Y.V., Yu, M.: Rusin Applied theory of elasticity, p. 319. Drofa, Moskow (2008)
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)
Russia Space Program and Exploration Handbook. – Vol. 1. Strategic Information, Developments and Regulations. – Washington: International Business Publications 305 p (2015)
Samarsky, A.A., Vabishchevich, V.P.: Computational heat transfer, Editorial USSR, 784 p (2003)
Sedelnikov, A.V.: Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. Russ. Aeronaut. 50(3), 322–325 (2007)
Sedelnikov, A.V.: Fractal quality of microaccelerations. Microgravity Sci. Technol. 24(5), 345–350 (2012)
Sedelnikov, A.V.: Control of microaccelerations as the major characteristics of space laboratory of specialized technological appointment as constructive methods, testing. Diagnistics. 7, 57–63 (2014)
Sedelnikov, A.V.: Modeling of microaccelerations caused by running of attitude-control engines of spacecraft with elastic structural elements. Microgravity Sci. Technol. 28(5), 491–498 (2016)
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)
Shen, Z., Li, H., Liu, X., et al.: Thermal shock induced dynamics of a spacecraft with a flexible deploying boom. Acta Astronaut. 141, 123–131 (2017)
Ushakov, I.B.: Advances of space medicine and biology research in Russia / I.B. Ilyin // 47th Session of the STS of the Committee on the Peaceful Uses of Outer Space. Vienna, Austria (2010)
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This work is supported by the Ministry of education and science of the Russian Federation in the framework of the State Assignments to higher education institutions and research organizations in the field of scientific activity (the project FSSS-2020-0017).
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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. Technol. 33, 22 (2021). https://doi.org/10.1007/s12217-020-09867-z
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DOI: https://doi.org/10.1007/s12217-020-09867-z