NASA Technical Reports Server (NASA) · 1993 · 12 citations · 0 references
EngineeringCombustion TheoryCeramic Matrix CompositesChemistryCeramic Matrix CompositeChemical EngineeringCombustion SynthesisDerivative ThermogravimetryThermodynamicsAdiabatic TemperatureThermoanalytical MethodMaterials ScienceCeramicsMetal-matrix CompositesHeat TransferHeterogeneous CombustionShs ReactionsCombustion ScienceCeramic SynthesisMetal-ceramic SystemsThermal EngineeringChemical Kinetics
Combustion synthesis or self-propagating high temperature synthesis (SHS) is effected by heating a reactant mixture, to above the ignition temperature (Tig) whereupon an exothermic reaction is initiated which produces a maximum or combustion temperature, Tc. These SHS reactions are being used to produce ceramics, intermetallics, and composite materials. One of the major limitations of this process is that relatively high levels of porosity, e.g., 50 percent, remain in the product. Conducting these SHS reactions under adiabatic conditions, the maximum temperature is the adiabatic temperature, Tad, and delta H (Tad) = 0, Tad = Tc. If the reactants or products go through a phase change, the latent heat of transformation needs to be taken into account.