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A torque, tension and stress corrosion evaluation of high strength A286 boltsThe problems associated with overtorque applied to the Booster Separation Motor (BSM) Igniter Adapter high strength 200 KSI (1379 Mpa) A286 CRES bolts and the threaded holes of the 7075-T73 aluminum alloy BSM cases are addressed. The evaluation included torque, tensile, and stress corrosion tests incorporating the A286 CRES bolts and the 7075-T73 aluminum alloy BSM cases. The tensile test data includes ultimate tensile load (UTL), Johnson's 2/3 yield load (J2/3YL), proportional limit load (PLL), and total bolt stretch. Torque tension data includes torque, torque induced load, and positive and negative break-away torque. Stress corrosion test data reflect the overtorque and the resulting torque induced loads sustained by the A286 CRES bolts torqued into a 7075-T73 aluminum alloy forged dome with threaded holes. After 60 days of salt fog exposure, the positive and the negative break-away torques, the subsequent mechanical property tensile test results, and the BSM dome threaded hole axial tensile pullout loads are reported.
Document ID
19860012479
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montano, J. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-86539
NAS 1.15:86539
Report Number: NASA-TM-86539
Report Number: NAS 1.15:86539
Accession Number
86N21950
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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