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NASA-LLIS-6196
Lessons Learned - Shaker Self-Check Unexpectedly Exceeded the Dynamic Test Limit
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:38:05Z | |
| date available | 2017-09-04T16:38:05Z | |
| date copyright | 40830 | |
| date issued | 2011 | |
| identifier other | VHLHOEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/101664 | |
| description abstract | Shaker system control software generates a self check immediately prior to a test at a signal level that is normally considered to be of insignificant strength compared to test levels. During a dynamic test of the Juno High Gain Antenna, however, the self check excited a response that exceeded the level from the subsequent test. In planning for dynamic testing, ensure that the self check signal will be set lower than any test level. | |
| language | English | |
| title | NASA-LLIS-6196 | num |
| title | Lessons Learned - Shaker Self-Check Unexpectedly Exceeded the Dynamic Test Limit | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2011 | |
| contenttype | fulltext | |
| subject keywords | Additional Categories.Flight Equipment | |
| subject keywords | Additional Categories.Ground Equipment | |
| subject keywords | Additional Categories.Hardware | |
| subject keywords | Additional Categories.Payloads | |
| subject keywords | Additional Categories.Spacecraft | |
| subject keywords | Additional Categories.Test & Verification | |
| subject keywords | Additional Categories.Test Article | |
| subject keywords | Additional Categories.Test Facility | |
| subject keywords | Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments | |
| subject keywords | Safety and Mission Assurance.Advanced planning of safety systems |
