درباره ما
NASA-LLIS-0713
Lessons Learned – Vehicle Integration/Tolerance Buildup Practices
Year: 2000
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.
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.
Show full item record
| 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 |