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Lessons Learned – Vehicle Integration/Tolerance Buildup Practices

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:54:48Z
date available2017-09-04T17:54:48Z
date copyright03/16/2000
date issued2000
identifier otherFIDEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/177904
description abstractPractice:
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.
languageEnglish
titleNASA-LLIS-0713num
titleLessons Learned – Vehicle Integration/Tolerance Buildup Practicesen
typestandard
page10
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext


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