Studies of NbC-WC solid solution-graphite composites
WC as densification aid for NbC-C composites, examining fabrication temperature, mechanical properties, solid solution composition, etc
Engineering topics
Publications and source records attributed to Harada, Y..
WC as densification aid for NbC-C composites, examining fabrication temperature, mechanical properties, solid solution composition, etc
Tungsten used in NbC-C composites as low melting densification additive to improve composite properties and lower fabrication temperatures
High temperature creep tests of niobium carbide- carbon composites, and evaluation of additives for tantalum carbide-carbon composites
Fabrication of metal carbide-graphite composites by hot pressing at high temperatures
Mechanical and thermodynamic properties of hot pressed tantalum carbide-graphite and niobium carbide-graphite composites
Physical and mechanical properties of tantalum carbide and niobium carbide composites
High strength, hot pressed metal carbide-graphite composites
Feasibility of fabricating graphite-metal carbide composites of high density and strength by hot pressing
Hot press fabrication effects on phase equilibrium and physical properties of refractory metal carbide-graphite composites
Liquid phase sintering in graphite-metal composites during hot pressing at high temperatures
Graphite effect on molybdenum-carbide composite properties and tungsten, vanadium, hafnium, tantalum, niobium, and zirconium metal systems
Coating pigment composed of zinc oxide and potassium silicate resists the effects of thermal shock and long exposure to direct sunlight.
Graphite-metal composites - hot pressing equipment modifications, hot pressing of calcined petroleum coke, and heterogeneity in density of niobium, hafnium, and molybdenum-graphites
In a previous research program for the Jet Propulsion- Laboratory, extensive studies led to the development and specifications of three zinc oxide-pigmented thermal-control coatings. The principal objectives of this program are: improvement of the three paints (as engineering materials), determination of the validity of our accelerated space-simulation testing, and continuation of the zinc oxide photolysis studies begun in the preceding program. Specific tasks that are discussed include: improvement of potassium silicate coatings as engineering materials and elucidation of their storage and handling problems; improvement of methyl silicone coatings as engineering materials; studies of zinc oxide photolysis to establish reasons for the observed stability of zinc oxide; and determination of space-simulation parameters such as long-term stability (to 8000 ESH), effect of coating surface temperature on the rate of degradation, and validity of accelerated testing (by reciprocity and wavelength dependency studies).
Stability of white spacecraft coatings subjected to ultraviolet radiation in vacuum
Development of space stable thermal control coatings
Stability of temperature-control coating materials to simulated space conditions of ultraviolet radiation
Radiation resistant white coatings for spacecraft