NASA-LLIS-0713
Lessons Learned – Vehicle Integration/Tolerance Buildup Practices
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:54:48Z | |
| date available | 2017-09-04T17:54:48Z | |
| date copyright | 03/16/2000 | |
| date issued | 2000 | |
| identifier other | FIDEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/177904 | |
| description abstract | Practice: Use master gauges, tooling, jigs, and fixtures to transfer precise dimensions to ensure accurate mating of interfacing aerospace hardware. Calculate overall worst-case tolerances using the root sum square method of element tolerances when integrating multiple elements of aerospace hardware. | |
| language | English | |
| title | NASA-LLIS-0713 | num |
| title | Lessons Learned – Vehicle Integration/Tolerance Buildup Practices | en |
| type | standard | |
| page | 10 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |

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