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NASA-LLIS-0729
Lessons Learned – Integration and Test Practices to Eliminate Stresses on Electrical and Mechanical Components
Year: 2000
Abstract: Practice:
Use proven GSFC practices during the integration and testing of flight hardware to prevent electrical and mechanical overstressing of flight hardware parts and components, thereby, assuring that the "designed in" reliability is not compromised.
Use proven GSFC practices during the integration and testing of flight hardware to prevent electrical and mechanical overstressing of flight hardware parts and components, thereby, assuring that the "designed in" reliability is not compromised.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:11:05Z | |
| date available | 2017-09-04T15:11:05Z | |
| date copyright | 03/31/2000 | |
| date issued | 2000 | |
| identifier other | LTCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/9437 | |
| description abstract | Practice: Use proven GSFC practices during the integration and testing of flight hardware to prevent electrical and mechanical overstressing of flight hardware parts and components, thereby, assuring that the "designed in" reliability is not compromised. | |
| language | English | |
| title | NASA-LLIS-0729 | num |
| title | Lessons Learned – Integration and Test Practices to Eliminate Stresses on Electrical and Mechanical Components | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |