NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Testing and evaluation of Vespel up to 450 deg F when used in nuts and bolts as a self-locking elementThe object of this investigation was to evaluate Vespel for potential application on the Solid Rocket Booster to replace all-metal deformed self-locking nuts and anchor nuts and be used as self-locking elements for bolts and screws. The Vespel self-locking elements were tested for prevailing torque retention at room temperature, after heating to 450 F and exposure for 3 hr, breakaway torque at 450 F and for vibration at a level consistent with the maximum expected on the SRB at lift-off and reentry. The investigation revealed Vespel has properties that can provide a self-locking capability for threaded fasteners up to 450 F and it can be used in nuts and anchor nuts for installation on the SRB. Vespel elements in bolts did not meet all our SRB requirements for reuse, however, we have defined a design for Vespel elements in nuts/anchor nuts that fully meets all requirements. It is recommended that No. 1, 1/4 in. and 5/16 in. nuts/anchor nuts be procured for use on the SRB. This system will eliminate the galling problems now encountered and achieve a much higher reuse life than the present deformed nut design.
Document ID
19840023569
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wood, C. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:86456
NASA-TM-86456
Report Number: NAS 1.15:86456
Report Number: NASA-TM-86456
Accession Number
84N31639
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available