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Goddard
Space Flight Center
1996 Phase I
Computer Code to Predict Fluid Flow Stability Of Capillary Pumped Loops
TTH Research, Inc.
Capitol Heights, MD
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INNOVATION
Implementation of recent, novel hydrodynamic-theoretical study. Improves
reliability of CPL design by predicting incidence of depriming behavior,
the main impediment to reliable operation
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Optional Powerpoint
file
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ACCOMPLISHMENTS
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Completed
mathematical model to perform nonlinear hydrodynamic stability analyses for
multiple pump/condenser CPL systems.
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Implemented model
in simplified computer code.
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COMMERCIALIZATION
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Computer model, for the first time, predicted unstable CPL flow regimes within which the system failed to operate.
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Successfully utilized to
analyze hydrodynamic stability characteristics of various
CPL systems including Terra Spacecrafts CPHTS,
CAPL-3 and HOST flight experiments.
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Incorporated into SINDA thermal analyzer to simulate on-orbit transient behaviors.
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GOVERNMENT/SCIENCE
APPLICATIONS
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Computer code has been in active
use at Goddard ever since for evaluating CPLs.
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For EOS-Terra, the results
of the code analysis indicated that the liquid line size
was too small under dynamic conditions even though it was
fine for steady state operation. Such a result was experimentally
verified in GSFC lab. Because of this finding, the EOS-Terra
project was convinced to enlarge the liquid line so as to mitigate
the risk.
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