| タイトル | Lessons from NASA |
| 著者（英） | Williams, W. C. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1981-10-01 |
| 言語 | eng |
| 内容記述 | Particular requirements related to the design and the operation of spacecraft have forced NASA to take a reliability approach that differs somewhat from that used in many other applications. NASA has found that some of the traditional tools of reliability engineering, such as life testing, reliability demonstration testing, maintainability analysis, and direct failure analysis, are impractical for spacecraft. In place of a statistical approach, the space agency uses an engineering approach to mission reliability. Reliability is to be obtained with the aid of three different approaches, including the application of effective design principles, the control and screening of all parts, and the testing of the entire spacecraft or its prototype for predicted capabilities. Attention is given to failure-mode analysis, the enhancement of Voyager reliability by autonomous operation, the redundancy in Shuttle design, the weeding out of bad hardware, and the preference for off-the-shelf devices. |
| NASA分類 | QUALITY ASSURANCE AND RELIABILITY |
| レポートNO | 81A49525 |
| 権利 | Copyright |
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