| タイトル | Composite Overwrapped Pressure Vessel (COPV) Stress Rupture Testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100021151 |
| 著者（英） | Leifeste, Mark R.; Saulsberry, Regor L.; Yoder, Tommy B.; Greene, Nathanael J.; Forth, Scott C.; Russell, Rick W.; Keddy, Chris P. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2010-05-19 |
| 言語 | eng |
| 内容記述 | This paper reports stress rupture testing of Kevlar(TradeMark) composite overwrapped pressure vessels (COPVs) at NASA White Sands Test Facility. This 6-year test program was part of the larger effort to predict and extend the lifetime of flight vessels. Tests were performed to characterize control parameters for stress rupture testing, and vessel life was predicted by statistical modeling. One highly instrumented 102-cm (40-in.) diameter Kevlar(TradeMark) COPV was tested to failure (burst) as a single-point model verification. Significant data were generated that will enhance development of improved NDE methods and predictive modeling techniques, and thus better address stress rupture and other composite durability concerns that affect pressure vessel safety, reliability and mission assurance. |
| NASA分類 | Structural Mechanics |
| レポートNO | JSC-CN-20720 |
| 権利 | No Copyright |
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