Design of Brayton rotating unit on rolling- element bearings
Design of Brayton rotating unit with roller bearings for space power system
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Design of Brayton rotating unit with roller bearings for space power system
Wind tunnel studies of scaled model of multijet cargo airplane
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Ball locking device which releases in response to small forces when subjected to high axial loads
Deployment systems for extending large area lightweight flexible solar arrays in space, tabulating estimated design weights including power-weight ratios
Antiwear and extreme pressure additive effects during bearing spinning with synthesized hydrocarbon oils
Solid lubricant applied to porous roller bearings prior to use in ultrahigh vacuum
Design and testing of 30 W/lb rollup subsolar array
Space erectable rollup solar array of arcuate solar panels furled on tapered drum for spacecraft storage during launch
Hardness and fatigue tests of steel bearing alloys
Synthesized hydrocarbon oil antiwear and extreme pressure additives effects on bearing spinning torque and endurance
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Monograph was published which summarizes and systematically orders large body of successful techniques and practices developed for design of liquid rocket engine turbopump bearings. Document was written to organize and present significant experience and knowledge accumulated by NASA in development and operational programs.
Short-term hot hardness studies were performed with five vacuum-melted steels at temperatures from 294 to 887 K (70 to 1140 F). Based upon a minimum Rockwell C hardness of 58, the temperature limitation on all materials studied was dependent on the initial room temperature hardness and the tempering temperature of each material. For the same room temperature hardness, the short-term hot hardness characteristics were identical and independent of material composition. An equation was developed to predict the short-term hardness at temperature as a function of initial room temperature hardness for AISI 52100, as well as the high-speed tool steels.