Compatibility analysis for the 1535-1660 MHz band, part 1 Final report, Jan. - Sep. 1969
Electromagnetic compatibility and radio frequency interference of aircraft radio antennas
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Electromagnetic compatibility and radio frequency interference of aircraft radio antennas
Thermal cycling tests of lithium fluoride compatibility with columbium base alloys
Determining compatible internal states of inverse automation by analysis of original automation
Compatibility and shielding analysis of science instruments in spacecraft containing radioisotope thermoelectric generator
Compatibility tests for spacecraft construction materials by specimen encapsulation with liquid rocket propellants
Compatibility during long term storage of liquid rocket propellants with spacecraft propulsion system materials
Injector compatibility improvement for Apollo lunar module descent engine ablative chamber
Compatibility conditions of theory of micromorphic elastic solids using Riemann theorem
Fluorinated lubricating oils and greases for use as liquid oxygen compatible lubricants, correlating stability and hydrogen substitution
Digital pulse optimization for space compatible electric connectors
Tensile and fatigue properties and liquid oxygen compatibility of bilaminate stainless steel-clad titanium prepared by vacuum deposition and explosive welding
Selection of materials for electrical connectors compatible with future space missions
Dry heat spacecraft sterilization-compatibility tests of reagents and growth media for planetary biological exploration
Power series uniformization by transformations of perturbation functions irregular part, considering compatibility problem
Procedures for achieving electromagnetic compatibility in electronic and electrical equipment for aerospace ground stations are investigated. The application of shielding theory to good design is treated and standards of good practice are outlined for bonding, grounding, wiring, and cabling. Some aspects of filter design are explained, and suggestions are given for the application of filters to electronic and electrical equipment.
Chemical compatibility between both pure and thoriated tungsten and uranium carbide alloys was studied at 1800 C for up to 3300 hours. Alloying with zirconium carbide appeared to widen the homogeneity range of uranium carbide, making additional carbon available for reaction with the tungsten. Reaction layers were formed both by vapor phase reaction and by physical contact, producing either or both UWC2 and W2C, dependent upon the phases present in the starting fuel alloy. Formation of UWC2 results in slow growth of the reaction layer with time, while W2C reaction layers grow rapidly, allowing equilibrium to be reached in less than 2500 hours at 1800 C. The presence of a thermal gradient had no effect on the reactions observed nor did the presence of thoria in the tungsten clad.
Results of compatibility tests between tungsten and hyperstoichiometric uranium carbide alloys run at 1800 C for 1000 and 2500 hours. These tests compared tungsten-buffered uranium carbide with tungsten-buffered uranium-zirconium carbide. The zirconium carbide addition appeared to widen the homogeneity range of the uranium carbide, making additional carbon available for reaction. Reaction layers could be formed by either of two diffusion paths, one producing UWC2, while the second resulted in the formation of W2C. UWC2 acts as a diffusion barrier for carbon and slows the growth of the reaction layer with time, while carbon diffusion is relatively rapid in W2C, allowing equilibrium to be reached in less than 2500 hours at a temperature of 1800 C.
Results of chemical compatibility tests between both pure tungsten and thoriated tungsten run at 1800 C for up to 3300 hours with uranium carbide alloys. Alloying with zirconium carbide appeared to widen the homogeneity range of uranium carbide, making additional carbon available for reaction with the tungsten. Reaction layers were formed both by vapor phase reaction and by physical contact, producing either or both UWC2 and W2C, depending upon the phases present in the starting fuel alloy. Formation of UWC2 results in slow growth of the reaction layer with time, while W2C reaction layers grow rapidly, allowing equilibrium to be reached in less than 2500 hours at 1800 C. Neither the presence of a thermal gradient nor the presence of thoria in the tungsten clad affect the reactions observed.