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Title: CARBONIZATION OF PLASTICS AND REFRACTORY MATERIALS RESEARCH

Technical Report ·
OSTI ID:4699795

Presented are the results of continuing investigations of the Carbonization of Plastics, Vapor Pressure of Refractory Materials, and Spectral Emmissivity of Refractories. Studies of thermal degradation of phenolic, epoxy, polyphemylene, and polymaphthalene resins were made with the arc-image furnace, the fluidized bed reactor, and the thermogravimetric analysis technique. The effect of semaicarbonized materials used as fillers has been studied and a Bendix time-of-flight mass spectrometer has been adapted to the study of transient and stable species resulting from the flash-photolysed degradation of plastics. Properties of carbom residue have been measured. Vapor pressure studies using the Langmuir evaporation technique, the matrix isolation method, and resonance line absorption spectroscopy have progressed. Rates of evaporation of tungsten carbides, hafnium carbide, amd titanium carbide have been measured; further conclusive measurements on zircomium carbide have been made. Preliminary application of the matrix isolatiom technique to thoria has been made. Resomance line absorption studies have been completed om zircomium carbide and titanium carbide and the accessible thermodynamic data have been deduced. Normal spectral emissivities of W-2 coated molybdemum, siliconized ATJ graphite, tantalum, molybdenum, tungsten carbide, and zirconium have been measured in the temperature range of 1400 to 3100 deg K. (auth)

Research Organization:
General Electric Co. Flight Propulsion Lab. Dept., Cincinnati
DOE Contract Number:
AF33(616)-6841
NSA Number:
NSA-17-041363
OSTI ID:
4699795
Report Number(s):
WADD-TR-60-646(Pt.II); AD-2979
Resource Relation:
Other Information: Orig. Receipt Date: 31-DEC-63
Country of Publication:
United States
Language:
English