Investigation of the process of maintaining the thermal regime of spacecraft on launch complexes with distributed circulation of coolant-Reference-Cited by-同舟云学术

Investigation of the process of maintaining the thermal regime of spacecraft on launch complexes with distributed circulation of coolant

Published:2021 Issue: Volume: Page:
ISSN:0094-243X
Container-title:XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration
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Author:

Matveeva Olga,Romanyak Alexander,Udovik Ilya

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0036467

Reference24 articles.

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2. Matveeva, O. P., Romanyak, A. Y., & Udovik, I. S. (2019). Analysis of energy saving options in the processes of maintaining the thermal modes of spacecraft at launch complexes. Engineering Journal: Science and Innovation, (12), 1–14.

3. Improving the processes of missile preparation at launch complexes on the basis of system design of interacting elements

4. Pironneau, O. (1994). Analysis of the K-Epsilon turbulence model. Wiley.

5. Shih, T. H., Liou, W. W., Shabbir, A., Yang, Z., & Zhu, J. (1994). A new k-epsilon eddy viscosity model for high Reynolds number turbulent flows: Model development and validation.

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