A theoretical investigation of the rolling motion of the nike cajun and nike apache rocket vehicles
Theoretical prediction of rolling motion of Nike-Cajun and Nike-Apache rocket vehicles
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Theoretical prediction of rolling motion of Nike-Cajun and Nike-Apache rocket vehicles
Rolling contact lubrication characteristics of polyphenyl ethers and mineral oils at reduced pressures
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Effects of cold rolling on mechanical properties of type 310 stainless steel at room and cryogenic temperatures
Fin trailing-edge wedge effect on Nike-Apache rocket roll history
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Rolling contact bearing lubrication and fatigue life in reduced pressure environment
Five-ball fatigue tester to investigate reduced pressure environment effect on rolling element fatigue life with polyphenyl ether
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The metallurgical results produced on balls tested in the rolling-contact fatigue spin rig were studied by metallographic examination. Origin and progression of fatigue failures were observed. These evaluations were made on SAE 52100 and AISI M-1 balls fatigue tested at room temperature (80 F) and 200 to 250 F. Most failures originated subsurface in shear; inclusions, structure changes, and directionalism adversely affected ball fatigue life. Structures in the maximum-shear-stress region of the balls of both materials were stable at room temperature and unstable at 200 to 250 F. Failures were of the same type as those found in full-scale bearings.
The rolling-contact fatigue spin rig was used to test groups of SAE 52100 9.16-inch-diameter balls lubricated with a mineral oil at 600,000-, 675,000-, and 750,000-psi maximum Hertz stress. Cylinders of AISI M-1 vacuum and commercial melts and MV-1 (AISI M-50) were used as race specimens. Stress-life exponents produced agree closely with values accepted in industry. The type of failure obtained in the spin rig was similar to the subsurface fatigue spells found in bearings.