For linear variation in propellant's thermal conductivity, stability criteria for propellant burning are derived; theoretical results indicate that stability modes are altered; stability diagrams are shown for two values in thermal conductivity parameter; thermal conductivity effect produces shift in instability modes from constant thermal conductivity condition; this effect is pronounced for values of dimensionless parameter b, less than one-third; in addition, low values of instability frequency are sensitive to thermal conductivity changes.
Thermal conductivity -- Parameter in solid propellant burning
AIAA J
AIAA Journal ; 4 , n 9 ; p 1610-1614
1966
5 pages
Article (Journal)
English
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