Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YDa/H44Mi
Repositorysid.inpe.br/iris@1916/2005/08.04.12.56   (restricted access)
Last Update2005:08.04.03.00.00 (UTC) administrator
Metadata Repositorysid.inpe.br/iris@1916/2005/08.04.12.56.23
Metadata Last Update2021:02.11.18.10.13 (UTC) administrator
Secondary KeyINPE-12923-PRE/8202
ISSN1359-4311
Citation KeyRiehlDutr:2005:DeExLo
TitleDevelopment of an experimental loop heat pipe for application in future space missions
Year2005
MonthJan.
Access Date2024, Apr. 28
Secondary TypePRE PI
Number of Files1
Size467 KiB
2. Context
Author1 Riehl, Roger R.
2 Dutra, T.
Group1 DMC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais, Divisão de Mecânica Espacial e Controle (INPE-DMC)
JournalApplied Thermal Engineering
Volume25
Number1
PagesApplied Thermal Engineering 25 (1): 101-112 Jan 2005
History (UTC)2005-08-04 12:56:24 :: sergio -> administrator ::
2006-09-28 22:30:02 :: administrator -> sergio ::
2008-01-07 12:52:54 :: sergio -> administrator ::
2021-02-11 18:10:13 :: administrator -> marciana :: 2005
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordsloop heat pipe
thermal control
capillary evaporator
two-phase flow
AbstractThe application of loop heat pipes (LHPs) as two-phase thermal control devices for space missions has been considered and successfully used in many spacecraft. Therefore, issues related to design, miniaturization of such a device and use of hazardous working fluids such as ammonia are still a concern. In order to face such concerns, this paper presents the development of an experimental LHP that deals with miniaturization and the use of an alternative working fluid. An experimental LHP was built and tested with acetone as the working fluid, designed to manage up to 70 W and using a capillary evaporator with reduced active length. The experimental results showed good thermal management performance of the proposed LHP for the imposed limitations to its design and operation. The proposed LHP presented to be a reliable thermal management device for application in future space missions, especially when considering the use of a less hazardous working fluid and the particular geometric characteristics. (C) 2004 Elsevier Ltd. All rights reserved.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Development of an...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filedevelopment experomental.pdf
User Groupadministrator
sergio
Visibilityshown
Copy HolderSID/SCD
Archiving Policydenypublisher denyfinaldraft24
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES.
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyright creatorhistory descriptionlevel documentstage doi e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype
7. Description control
e-Mail (login)marciana
update 


Close