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タイトルProficiency Testing for Evaluating Aerospace Materials Test Anomalies
本文(外部サイト)http://hdl.handle.net/2060/20080026114
著者(英)Peyton, S.; Hirsch, D.; Beeson, H.; Motto, S.
著者所属(英)NASA Johnson Space Center
発行日2006-10-18
言語eng
内容記述ASTM G 86 and ASTM G 74 are commonly used to evaluate materials susceptibility to ignition in liquid and gaseous oxygen systems. However, the methods have been known for their lack of repeatability. The inherent problems identified with the test logic would either not allow precise identification or the magnitude of problems related to running the tests, such as lack of consistency of systems performance, lack of adherence to procedures, etc. Excessive variability leads to increasing instances of accepting the null hypothesis erroneously, and so to the false logical deduction that problems are nonexistent when they really do exist. This paper attempts to develop and recommend an approach that could lead to increased accuracy in problem diagnostics by using the 50% reactivity point, which has been shown to be more repeatable. The initial tests conducted indicate that PTFE and Viton A (for pneumatic impact) and Buna S (for mechanical impact) would be good choices for additional testing and consideration for inter-laboratory evaluations. The approach presented could also be used to evaluate variable effects with increased confidence and tolerance optimization.
NASA分類Composite Materials
権利Copyright, Distribution as joint owner in the copyright


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