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Study of longitudinal heat transfer in low temperature heat pipes with axial grooves and discrete metal fibers for space thermal control systems

Baturkin, Volodymyr und Ho, Tra-Mi (2016) Study of longitudinal heat transfer in low temperature heat pipes with axial grooves and discrete metal fibers for space thermal control systems. 14th International Conference on Simulation and Experiments in Heat Transfer and its Application, 07.-09.09.2016, Ancona, Italy.

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Kurzfassung

Development of space thermal control (TC) technique is tightly connected with achievements of heat pipe (HP) science and technology. The paper presents the experimental results of heat transfer for the following perspective HP designs with round cross section in wide range of operation parameters: saturation vapor temperature -70…+60 C, transferred heat power 0.5-100 W, axial heat flux density 10-250 W/cm2: a Copper – methanol HP with cooper discrete metal fiber capillary structure, external diameter 0.006 m, type – variable thermal conductance b Stainless steel – methanol HP with cooper discrete metal fiber capillary structure, external diameter 0.008 m, type- variable thermal conductance c Aluminum –ammonia HP with axial grooved capillary structure, external diameter 0.012 m, type- constant thermal conductance As characteristic parameter for comparison the ratio R=(T1-T2)/Q is used, where Q- transferred heat power, T1, T2 – averaged temperature of heat input and output zones of heat pipe. HPs “a” have shown essential impact of T2 of R, which varies from 60 K/W to 0.5 K/W. Physical basis of such behavior deals with changing of vapor flow regime in inner space and with the change of intensity of heat transfer by saturation vapor pressure. For HP “b” parameter R has variation from 90 K/W to 4 K/W. Physical basis of such behavior deals with creation of vapor –noncondensible gas boundary in coldest part of heat pipe and as the sequence, with variation of intensity of heat transfer. For HP “c” parameter R varies from 0.06 K/W to 0.045 K/W. Change of T2 has no essential impact of HP thermal resistance R. Comparison of longitudinal heat transfer characteristics of different types of heat pipes, obtained on representative quantity of tested units, allowed to define their functional abilities and duties in TC for different space applications.

elib-URL des Eintrags:https://elib.dlr.de/104435/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Study of longitudinal heat transfer in low temperature heat pipes with axial grooves and discrete metal fibers for space thermal control systems
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Baturkin, Volodymyrvolodymyr.baturkin (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Ho, Tra-MiDLR-Bremen, tra-mi.ho (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:Mai 2016
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Name der Reihe:WIT eLibrary (www.witpress.com)
Status:akzeptierter Beitrag
Stichwörter:space, thermal control, heat pipe, study
Veranstaltungstitel:14th International Conference on Simulation and Experiments in Heat Transfer and its Application
Veranstaltungsort:Ancona, Italy
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:07.-09.09.2016
Veranstalter :WESSEX INSTITUTE, UK and Lund University, Sweden
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Technik für Raumfahrtsysteme
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R SY - Technik für Raumfahrtsysteme
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt Mascot (Bus)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme
Hinterlegt von: Baturkin, Volodymyr
Hinterlegt am:31 Mai 2016 12:17
Letzte Änderung:31 Mai 2016 12:20

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