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NASA-LLIS-0824
Lessons Learned – Space Radiation Effects on Electronic Components in Low-Earth Orbit
Year: 2000
Abstract: Practice:
During system design, choose electronic components/devices which will provide maximum failure tolerance from Space Radiation Effects. The information above provides guidance in selection of radiation hardened (rad-hard) solid state devices and microcircuits for use in space vehicles which operate in low-earth orbits.
During system design, choose electronic components/devices which will provide maximum failure tolerance from Space Radiation Effects. The information above provides guidance in selection of radiation hardened (rad-hard) solid state devices and microcircuits for use in space vehicles which operate in low-earth orbits.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:17:56Z | |
| date available | 2017-09-04T16:17:56Z | |
| date copyright | 04/18/2000 | |
| date issued | 2000 | |
| identifier other | TEDEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/81388 | |
| description abstract | Practice: During system design, choose electronic components/devices which will provide maximum failure tolerance from Space Radiation Effects. The information above provides guidance in selection of radiation hardened (rad-hard) solid state devices and microcircuits for use in space vehicles which operate in low-earth orbits. | |
| language | English | |
| title | NASA-LLIS-0824 | num |
| title | Lessons Learned – Space Radiation Effects on Electronic Components in Low-Earth Orbit | en |
| type | standard | |
| page | 8 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |