Combustion Characteristics of Crystalline Rocket Oxidizers.
DELAWARE UNIV NEWARK DEPT OF CHEMISTRY
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The report describes a combustion research and testing program that has achieved one of its long range goals that of providing new theory and practice for burning rate control of solid rocket propellants. In addition, new understanding has been added of the role played by the crystalline oxidizers used in those propellants. Author
- Combustion and Ignition
- Solid Rocket Propellants