Journal of Siberian Federal University. Engineering & Technologies / Numerical Study of the Characteristics of Heat Pipes in the Composition Electronic Equipment of Spacecraft

Full text (.pdf)
Issue
Journal of Siberian Federal University. Engineering & Technologies. 2015 8 (6)
Authors
Kulagin, Vladimir A.; Sokolov, Nikita Y.
Contact information
Kulagin, Vladimir A.:Siberian Federal University 79 Svobodny, Krasnoyarsk, 660041, Russia; E-mail: ; Sokolov, Nikita Y.:siberian Federal University 79 Svobodny, Krasnoyarsk, 660041, Russia; AO «Information Satellite Systemsthem Academician M.F. Reshetnev» 52 Lenin Str., Zheleznogorsk, 662972, Russia
Keywords
flat heat pipe; spacecraft; mathematical model; heat transfer fluid
Abstract

T-shaped planar heat pipe (HP) is designed for use in the construction of spacecraft (SC). The article presents the developed mathematical model for calculating the thermal regime of the product using flat heat pipes, based on the solution of two-dimensional stationary equations of a of mass conservation, supplemented Darcy equations for fluid and vapor. For a given location heat sources and sinks on the surface of the flat heat pipe calculated distribution of pressure and mass flows for both phases of the coolant. Analysis of of working capacity of the heat pipe to the set conditions based on verification of the capillary restriction

Pages
769-773
Paper at repository of SibFU
https://elib.sfu-kras.ru/handle/2311/19843

Creative Commons License This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).