@Article{RiehlDutr:2005:DeExLo,
author = "Riehl, Roger R. and Dutra, T.",
affiliation = "Instituto Nacional de Pesquisas Espaciais, Divis{\~a}o de
Mec{\^a}nica Espacial e Controle (INPE-DMC)",
title = "Development of an experimental loop heat pipe for application in
future space missions",
journal = "Applied Thermal Engineering",
year = "2005",
volume = "25",
number = "1",
pages = "Applied Thermal Engineering 25 (1): 101--112 Jan 2005",
month = "Jan.",
keywords = "loop heat pipe, thermal control, capillary evaporator, two-phase
flow.",
abstract = "The 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.",
copyholder = "SID/SCD",
issn = "1359-4311",
language = "en",
targetfile = "development experomental.pdf",
urlaccessdate = "16 jun. 2024"
}