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Refractory Metal Heat Pipe Life Test - Test Plan and Standard Operating ProceduresRefractory metal heat pipes developed during this project shall be subjected to various operating conditions to evaluate life-limiting corrosion factors. To accomplish this objective, various parameters shall be investigated, including the effect of temperature and mass fluence on long-term corrosion rate. The test series will begin with a performance test of one module to evaluate its performance and to establish the temperature and power settings for the remaining modules. The performance test will be followed by round-the-clock testing of 16 heat pipes. All heat pipes shall be nondestructively inspected at 6-month intervals. At longer intervals, specific modules will be destructively evaluated. Both the nondestructive and destructive evaluations shall be coordinated with Los Alamos National Laboratory. During the processing, setup, and testing of the heat pipes, standard operating procedures shall be developed. Initial procedures are listed here and, as hardware is developed, will be updated, incorporating findings and lessons learned.
Document ID
20110004376
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Martin, J. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Reid, R. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TP-2010-216452
M-1301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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