Method of improving the reliability of a rolling element system Patent
Improving load capacity and fatigue life of rolling element systems in rockets and missiles
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Improving load capacity and fatigue life of rolling element systems in rockets and missiles
Rolling element fatigue lives of AISI T-1, AISI M-42, AISI 52,100, and Halmo at 150 F
Investigating fatigue life of rolling elements at 150 F and 800,000 psi
Fluidic roll control for Aerobee rocket vehicle
Roll-control effectiveness of spoiler configurations on aircraft model with variable sweep wings at supersonic speeds
Test of rolling element fatigue life with fluorinated ether lubricant at cryogenic temperature using five ball fatigue tester
Elastohydrodynamic film thickness between rolling disks with synthetic paraffinic oil at temperatures from 339 to 589 K
Analysis of coupled roll-spiral-mode, pilot induced oscillation occurring with M-2F2 lifting body
Single degree of freedom roll response due to vertical random two dimensional vertical gusts
Rolling ball fatigue and lubrication with fluorinated polyethers at cryogenic temperatures compared to superfined mineral oil
Launch vehicle under influence of random fin misalignments, predicting roll rate by statistical analysis
Ocular counter-rolling as otolith organ function indicator
Cone roll dynamics-ablation patterns coupling in hypersonic wind tunnels
Method introduces roll into the flying-spot scanner by modifying the scanning waveforms.
A program to develop a 250 square foot roll-up solar array with a power-to-weight ratio exceeding 30 watts per pound is described. The system design and fabrication of a full scale engineering development model are discussed. The system and development test program results are presented. Special test equipment and test procedures are included, together with comparisons of experimental and analytical results.
Equations of lifting entry are considered for fixed-angle-of-attack vehicular motion with path control for roll modulation of lift. Attention is directed to relocation and its consequences for the fixed-angle-of-attack atmospheric entry problem. Two reduced-order methods for working with the resulting system of equations are briefly examined. The methods are deemed to warrant further study.
Auto-vacuum cleaning technique was applied to titanium parts prior to welding. This provides oxide-free welding surfaces. Diffusion welding can be accomplished in as little as five minutes of hot pressing. Roll welding can be accomplished with only ten percent deformation.
Analysis was made to determine correlation between number and size of carbide particles and rolling-element fatigue. Correlation was established, and carbide factor was derived that can be used to predict fatigue life more effectively than such variables as heat treatment, chemical composition, and hardening mechanism.