Abstract
A thermal model for the aluminized polymer shell of a gauge-alignment spacecraft was developed to calculate the steady-state temperature distribution of this shell at a fixed orientation to the Sun. A modified version of the model was used to analyze the quasistationary distribution of the shell temperature in the case of its rotation with a constant angular velocity about an axis perpendicular the direction to the Sun.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
Small Information Support Spacecrafts (Radiotekhnika, Moscow, 2010) [in Russian].
Rockets and Spacecrafts Designed by the Yuzhnoe Design Bureau (Yangel Yuzhnoe State Design Bureau, Dnepropetrovsk, 2000) [in Russian].
M. V. Tarasenko, Military Aspects of the Soviet Space Program (Nikol’, Moscow, 1992) [in Russian].
M. A. Komkov, Yu. Z. Bolotin, and T. V. Vasil’eva, “Determination of Structural and Technological Parameters of Pipelines Made by Winding of Polyimide Film,” Nauka Obrazovanie, No. 3, 169–178 (2013); DOI: 10.7463/0313.0541990.
Spacecraft Thermal Control Handbook, Vol. 1: Fundamental Technologies (Aerospace Press, El Segundo, 2002).
V. S. Zarubin and G. N. Kuvyrkin, “Mathematical Modeling of Thermomechanical Processes under Intense Thermal Action,” Teplofiz. Vysok. Temp. 41 (2), 300–309 (2003).
V. N. Zimin, “On the Simulation and Calculation of the Dynamics of Deployment of Deployable Space Structures,” Oboron. Tekh., No. 1, 123–127 (2006).
V. S. Avduevskii, B. M. Galitseiskii, G. A. Glebov, Yu. I. Danilov, et al., Fundamentals of Heat Transfer in Aviation and Space Engineering (Mashinstroenie, Moscow, 1975) [in Russian].
R. Siegel and J. R. Howell, Thermal Radiation Heat Transfer (Hemisphere, New York, 1992).
M. A. Komarova, “Temperature Conditions in the Node Housing in an Autonomous Flight to the International Space Station,” Izv. Ross. Akad. Nauk, Energetika, No. 2, 23–30 (2012).
A. A. Gukalo and A. S. Gribkov, “Temperature Optimization of a Flat and Cruciform Refrigerator Emitter of a Space Nuclear Power Plant with the External Thermal Radiation Taken into Account,” Izv. Ross. Akad. Nauk, Energetika, No. 2, 103–110 (2012).
“The Degree of Blackness and the Solar Radiation Absorption Coefficients of Aluminum and Alloys,” http://forca.ru/spravka/shiny-i-tokoprovody/stepen-chernoty-i-koefficienty-pogloscheniya-solnechnoy-radiaciialyuminiem-i-splavami.html.
V. S. Zarubin, “Temperature State of a Thin Spherical Shell,” Prikl. Mekh. Tekh. Fiz., No. 6, 169–171 (1963).
“Analytical Portal of the Chemical Industry,” http://www.newchemistry.ru/production.phpcat-id=52&catparent= 7&level=3.
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © V.S. Zarubin, V.N. Zimin, G.N. Kuvyrkin.
Rights and permissions
About this article
Cite this article
Zarubin, V.S., Zimin, V.N. & Kuvyrkin, G.N. Temperature Distribution in the Spherical Shell of a Gauge-Alignment Spacecraft. J Appl Mech Tech Phy 58, 1083–1090 (2017). https://doi.org/10.1134/S0021894417060141
Received:
Revised:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0021894417060141