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NASA-LLIS-0676
Lessons Learned – Electrical, Electronic and Electromechanical (EEE) Parts Derating
Year: 2000
Abstract: Practice:
Derate applied stress levels for electrical, electronic, and electromechanical (EEE) part characteristics and parameters with respect to the maximum stress level ratings of the part. The allowed stress levels are established as the maximum levels in circuit applications.
Derate applied stress levels for electrical, electronic, and electromechanical (EEE) part characteristics and parameters with respect to the maximum stress level ratings of the part. The allowed stress levels are established as the maximum levels in circuit applications.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:37:43Z | |
| date available | 2017-09-04T18:37:43Z | |
| date copyright | 03/09/2000 | |
| date issued | 2000 | |
| identifier other | JOCEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/219551 | |
| description abstract | Practice: Derate applied stress levels for electrical, electronic, and electromechanical (EEE) part characteristics and parameters with respect to the maximum stress level ratings of the part. The allowed stress levels are established as the maximum levels in circuit applications. | |
| language | English | |
| title | NASA-LLIS-0676 | num |
| title | Lessons Learned – Electrical, Electronic and Electromechanical (EEE) Parts Derating | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |