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