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NASA-LLIS-0781
Lessons Learned - Thermal-Vacuum Versus Thermal-Atmospheric Tests of Electronic Assemblies
Year: 2000
Abstract: Practice:
Perform all thermal environmental tests on electronic spaceflight hardware in a flight-like thermal vacuum environment (i.e., do not substitute an atmospheric pressure thermal test for the thermal/ vacuum test). Moreover, if a compromise is thought to be necessary for nontechnical reasons, then an analysis is required to quantify the reduction in test demonstrated reliability.
Perform all thermal environmental tests on electronic spaceflight hardware in a flight-like thermal vacuum environment (i.e., do not substitute an atmospheric pressure thermal test for the thermal/ vacuum test). Moreover, if a compromise is thought to be necessary for nontechnical reasons, then an analysis is required to quantify the reduction in test demonstrated reliability.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:20:43Z | |
| date available | 2017-09-04T15:20:43Z | |
| date copyright | 04/14/2000 | |
| date issued | 2000 | |
| identifier other | MXCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/20641 | |
| description abstract | Practice: Perform all thermal environmental tests on electronic spaceflight hardware in a flight-like thermal vacuum environment (i.e., do not substitute an atmospheric pressure thermal test for the thermal/ vacuum test). Moreover, if a compromise is thought to be necessary for nontechnical reasons, then an analysis is required to quantify the reduction in test demonstrated reliability. | |
| language | English | |
| title | NASA-LLIS-0781 | num |
| title | Lessons Learned - Thermal-Vacuum Versus Thermal-Atmospheric Tests of Electronic Assemblies | en |
| type | standard | |
| page | 7 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |