| タイトル | ANSI/AIAA S-081A, Pressure Vessel Standards Implementation Guidelines |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090037553 |
| 著者（英） | Greene, Nathanael J. |
| 著者所属（英） | NASA White Sands Test Facility |
| 発行日 | 2009-08-06 |
| 言語 | eng |
| 内容記述 | The stress rupture specification for Composite Overwrapped Pressure Vessels (COPV) is discussed. The composite shell of the COPV shall be designed to meet the design life considering the time it is under sustained load. A Mechcanical Damage Control Plan (MDCP) shall be created and implemented that assures the COPV will not fail due to mechanical damage due to manufacturing, testing, shipping, installation, or flight. Proven processes and procedures for fabrication and repair shall be used to preclude damage or material degradation during material processing, manufacturing operations, and refurbushment.Selected NDI techniques for the liner and/or boss(es) shall be performed before overwrapping with composite. When visual inspection reveals mechanical damage or defects exceeding manufacturing specification levels (and standard repair procedures), the damaged COPV shall be submitted to a material review board (MRB) for disposition. Every COPV shall be subjected to visual and other non-destructive inspection (NDI), per the inspection plan. |
| NASA分類 | Composite Materials |
| 権利 | No Copyright |
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