Loop heat pipes and capillary pumped loops-an applications perspective
Author(s) -
Dan Butler,
Jentung Ku,
Theodore D. Swanson
Publication year - 2002
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.1449707
Subject(s) - accumulator (cryptography) , heat pipe , spacecraft , loop (graph theory) , loop heat pipe , evaporator , heat transfer , perspective (graphical) , capillary action , computer science , feedback loop , mechanical engineering , systems engineering , aerospace engineering , engineering , physics , mechanics , meteorology , mathematics , combinatorics , artificial intelligence , computer security , heat exchanger , algorithm
Capillary pumped loops (CPLs) and loop heat pipes (LHPs) are versatile two-phase heat transfer devices which have recently gained increasing acceptance in space applications. Both systems work based on the same principles and have very similar designs. Nevertheless, some differences exist in the construction of the evaporator and the hydro-accumulator, and these differences lead to very distinct operating characteristics for each loop. This paper presents comparisons of the two loops from an applications perspective, and addresses their impact on spacecraft design, integration, and test. Some technical challenges and issues for both loops are also addressed.
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom