| Issue |
MATEC Web Conf.
Volume 179, 2018
2018 2nd International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2018)
|
|
|---|---|---|
| Article Number | 03019 | |
| Number of page(s) | 6 | |
| Section | Aerospace | |
| DOI | https://doi.org/10.1051/matecconf/201817903019 | |
| Published online | 26 July 2018 | |
Analysis of Operation of Throttle Micro-cooler at Nitrogen Use with Near-critical Parameters
Department of Heat Engineering and Heat Engines, Samara University, 443086, Moskovskoye shosse, 34, Samara, Russia
a Corresponding author: dmitry.uglanov@mail.ru
The work of a throttle cooling system with a standard balloon and a throttle cooling system from a cryogenic filling balloon is considered. A comparison between the geometric and hydraulic characteristics of the micro heat exchangers of the two systems is made. The prospects of using the latest system for cooling of photodetector devices (PD) of the infrared range of navigation and research systems for aerospace applications are also shown.
© The Authors, published by EDP Sciences 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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