NASA NTRS · 19650011392
Effect of oxidizer particle size on solid- propellant combustion stability
Abstract
Oxidizer particle size effect on solid propellant combustion stability
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Morrell, G., Pinns, M. L.. 1965-04-01. Effect of oxidizer particle size on solid- propellant combustion stability. https://ntrs.nasa.gov/citations/19650011392
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