NASA SBIR SUCCESS STORY Goddard Space Flight Center
1996 Phase I

Computer Code to Predict Fluid Flow Stability Of Capillary Pumped Loops

TTH Research, Inc.

Capitol Heights, MD

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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ACCOMPLISHMENTS
    • Completed mathematical model to perform nonlinear hydrodynamic stability analyses for multiple pump/condenser CPL systems.
    • Implemented model in simplified computer code.
COMMERCIALIZATION
    • Computer model, for the first time, predicted unstable CPL flow regimes within which the system failed to operate.
    • Successfully utilized to analyze hydrodynamic stability characteristics of various CPL systems including Terra Spacecraft’s CPHTS, CAPL-3 and HOST flight experiments.
    • Incorporated into SINDA thermal analyzer to simulate on-orbit transient behaviors.
GOVERNMENT/SCIENCE APPLICATIONS
    • Computer code has been in active use at Goddard ever since for evaluating CPLs.
    • 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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