Mathematical simulation of heat exchange in a nonhermetic instrumental compartment of a spacecraft
Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonher...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Burakov, V. A. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2000 |
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| Schlagwörter: |
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| Anmerkung: |
© Kluwer Academic/Plenum Publishers 2000 |
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| Übergeordnetes Werk: |
Enthalten in: Journal of engineering physics and thermophysics - Springer US, 1992, 73(2000), 1 vom: Jan., Seite 112-123 |
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| Übergeordnetes Werk: |
volume:73 ; year:2000 ; number:1 ; month:01 ; pages:112-123 |
| Links: |
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| DOI / URN: |
10.1007/BF02681685 |
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| Katalog-ID: |
OLC2060362229 |
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| 520 | |a Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments. | ||
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10.1007/BF02681685 doi (DE-627)OLC2060362229 (DE-He213)BF02681685-p DE-627 ger DE-627 rakwb eng 530 VZ 52.00 bkl Burakov, V. A. verfasserin aut Mathematical simulation of heat exchange in a nonhermetic instrumental compartment of a spacecraft 2000 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic/Plenum Publishers 2000 Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments. Heat Exchange Geostationary Orbit Radiative Heat Exchange Radiator Panel Honeycomb Panel Korchagin, E. N. aut Kozhukhov, V. P. aut Tkachenko, A. S. aut Shcherbakov, I. V. aut Enthalten in Journal of engineering physics and thermophysics Springer US, 1992 73(2000), 1 vom: Jan., Seite 112-123 (DE-627)131134892 (DE-600)1124753-8 (DE-576)032746717 1062-0125 nnns volume:73 year:2000 number:1 month:01 pages:112-123 https://doi.org/10.1007/BF02681685 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-PHY GBV_ILN_70 GBV_ILN_2416 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4700 52.00 VZ AR 73 2000 1 01 112-123 |
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Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments. © Kluwer Academic/Plenum Publishers 2000 |
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Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments. © Kluwer Academic/Plenum Publishers 2000 |
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Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments. © Kluwer Academic/Plenum Publishers 2000 |
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A.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Mathematical simulation of heat exchange in a nonhermetic instrumental compartment of a spacecraft</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2000</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Kluwer Academic/Plenum Publishers 2000</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Heat Exchange</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Geostationary Orbit</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Radiative Heat Exchange</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Radiator Panel</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Honeycomb Panel</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Korchagin, E. 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