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This document provides criteria for the design and analysis of preloaded bolts used in Space Shuttle joints. It defines key terms like limit load, preload, and joint separation load. It also outlines requirements and procedures for calculating maximum and minimum expected preloads, checking bolt strength, preventing joint separation, and ensuring adequate fatigue life. The criteria is intended to standardize the consistent evaluation of preloaded bolts throughout the Space Shuttle Program.

Author

ffontana

Language

EN