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Selecting a thermodynamic cycle for the closed gas-turbine power plant of spacecraft in order to minimize surface of the cooler-radiator

Crossref DOI link: https://doi.org/10.1134/S0018151X14040014

Published Online: 2014-08-15

Published Print: 2014-07

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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