NASA-LLIS-0342
Lessons Learned - Critical Hardware Functional Verification
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:08:29Z | |
| date available | 2017-09-04T18:08:29Z | |
| date copyright | 08/09/1994 | |
| date issued | 1994 | |
| identifier other | GSAEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/191524 | |
| description abstract | Description of Driving Event: On the STS 51/TOS mission, during payload deployment, commands intended to initiate only the primary SUPER*ZIP explosive cord actually resulted in the simultaneous firing of both the primary explosive cord and back-up explosive cord. This simultaneous explosive cord firing resulted in the rupture of a SUPER*ZIP containment tube and the release of contaminants and high energy debris into the orbiter cargo bay. | |
| language | English | |
| title | NASA-LLIS-0342 | num |
| title | Lessons Learned - Critical Hardware Functional Verification | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1994 | |
| contenttype | fulltext | |
| subject keywords | Energetic Materials - Explosive/Propellant/Pyrotechnic | |
| subject keywords | Hardware | |
| subject keywords | Safety & Mission Assurance | |
| subject keywords | Test & Verification |

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