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NASA-LLIS-0766
Lessons Learned - Reliability Considerations for Launch Vehicle Command Destruct Systems
Year: 2000
Abstract: Practice:
Use built-in redundancies, safe and arm provisions, approved and qualified initiators and detonators, shaped charge development testing to collect empirical data for design (empirical testing), and failsafe designs to achieve reliability in launch vehicle command destruct systems.
Use built-in redundancies, safe and arm provisions, approved and qualified initiators and detonators, shaped charge development testing to collect empirical data for design (empirical testing), and failsafe designs to achieve reliability in launch vehicle command destruct systems.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:03:51Z | |
| date available | 2017-09-04T17:03:51Z | |
| date copyright | 04/06/2000 | |
| date issued | 2000 | |
| identifier other | BYCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/127424 | |
| description abstract | Practice: Use built-in redundancies, safe and arm provisions, approved and qualified initiators and detonators, shaped charge development testing to collect empirical data for design (empirical testing), and failsafe designs to achieve reliability in launch vehicle command destruct systems. | |
| language | English | |
| title | NASA-LLIS-0766 | num |
| title | Lessons Learned - Reliability Considerations for Launch Vehicle Command Destruct Systems | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |