An effect of oxidizer particle size on combustion stability in composite propellants
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 2000 ; Las Vegas , NV , U.S.A.
01.01.2000
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
An Effect of Oxidizer Particle Size on Combustion Stability in Composite Propellants
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