Optimal way for choosing parameters of spacecraft’s screen-vacuum heat insulation
- Authors: Formalev V.F.1, Kolesnik S.A.1, Selin I.A.1, Kuznetsova E.L.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 55, No 1 (2017)
- Pages: 101-106
- Section: Heat and Mass Transfer and Physical Gasdynamics
- URL: https://journals.rcsi.science/0018-151X/article/view/157045
- DOI: https://doi.org/10.1134/S0018151X17010096
- ID: 157045
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