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NASA-LLIS-6636
Conduct a Final Mechanical Walkdown Prior to Spacecraft Integration with the Launch Vehicle
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:08:41Z | |
| date available | 2017-09-04T18:08:41Z | |
| date copyright | 41207 | |
| date issued | 2012 | |
| identifier other | GSJYAFAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/191671 | |
| description abstract | Where previous JPL spaceflight projects relied solely on interim inspections and walkdowns during ATLO, the in-house MSL project conducted a formal, final, mechanical walkdown of the as-built configuration prior to vehicle stacking at the launch site. Because NuSTAR was an out-of-house build, an assessment and final walkdown was performed independent of the system contractor that similarly produced findings and observations. Conduct a final mechanical walkdown of the spacecraft prior to stacking or encapsulation for launch. | |
| language | English | |
| title | NASA-LLIS-6636 | num |
| title | Conduct a Final Mechanical Walkdown Prior to Spacecraft Integration with the Launch Vehicle | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2012 | |
| contenttype | fulltext |
