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Erosive burning of composite solid propellants
Combustion and Flame, 1966A model is proposed for erosive burning of ammonium perchlorate composite wolid propellants. It is assumed that combustion takes place in the turbulent boundary layer and that the turbulent flame consists of distorted ‘flamelets’ but otherwise retains on a molecular scale the characteristics of a laminar flame.
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A Review on the Use of Burning Rate Suppressants in AP‐Based Composite Propellants
Propellants, Explosives, Pyrotechnics, 2022Shuang Xu, Jie Kong
exaly
An Overview of Composite Propellant Burning
International Journal of Engineering Trends and Technology, 2015A. M Hegab, S. A Gutub
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SYNOPTIC: Composite Propellant Combustion
AIAA Journal, 1970R. L. DERR, J. R. OSBORN
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