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Using of heat-pipes with increased heat conduction as core elements of system of thermal control for aerospace equipment
- Authors: 1, 2, 3
-
Affiliations:
- State Research and Production Space Rocket Center «TsSKB-Progress»
- Samara State University
- State Scientific Production Space-Rocket Centre “TsKB Progress”
- Issue: Vol 8, No 3-2 (2009): Special Issue
- Pages: 98-101
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/741
- DOI: https://doi.org/10.18287/2541-7533-2009-0-3-2(19)-98-101
- ID: 741
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Abstract
This paper, executed under the direction of doctor of engineerings sciences, professor of Biryuka Vladimir Vasil'evicha, studies the main thermal physic characteristics of heat-pipes with increased heat conduction, which have axial grooves made of aluminum alloy AD31 as wick.
About the authors
State Research and Production Space Rocket Center «TsSKB-Progress»
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
Samara State University
Email: sadohina@ssau.ru
Russian Federation
State Scientific Production Space-Rocket Centre “TsKB Progress”
Email: sadohina@ssau.ru
Russian Federation
References
- Кузнецов, Н.Д. Акустика газовых потоков турбореактивных двухконтурных двигателей: учеб. Пособие / Н.Д. Кузнецов, И.С. Загузов, А.П. Комаров. – Уфа, УАИ, 1984. – 101 с.
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