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Teplofizika vysokikh temperatur, 2014, Volume 52, Issue 4, Pages 613–616
DOI: https://doi.org/10.7868/S0040364414040012 (Mi tvt629) 		 
This article is cited in 6 scientific papers (total in 6 papers)

High Temperature Apparatuses and Structures

Selecting a Thermodynamic Cycle for the Closed Gas Turbine Power Plant of Spacecraft in Order to Minimize Surface of the Cooler-Radiator

A. N. Arbekov

N. E. Bauman Moscow State Technical University
Full-text PDF (160 kB) Citations (6)
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DOI: https://doi.org/10.7868/S0040364414040012
Abstract: The influence of the thermodynamic cycle scheme selected for a closed gas-turbine power plant of spacecraft on the specific surface of its cooler-radiator are evaluated. The dependence of the cooler-radiator characteristics on the regeneration, intermediate cooling, and heating of the working medium are analyzed.
Received: 03.07.2013
English version:
High Temperature, 2014, Volume 52, Issue 4, Pages 584–587
DOI: https://doi.org/10.1134/S0018151X14040014
Bibliographic databases:
Document Type: Article
UDC: 621.165
Language: Russian
Citation: A. N. Arbekov, “Selecting a Thermodynamic Cycle for the Closed Gas Turbine Power Plant of Spacecraft in Order to Minimize Surface of the Cooler-Radiator”, TVT, 52:4 (2014), 613–616; High Temperature, 52:4 (2014), 584–587
Citation in format AMSBIB
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    • This publication is cited in the following 6 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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