Combustion Mechanisms of AN/AP Mixed-Oxidizer Composite Propellants
33rd, Joint propulsion conference ; 1997 ; Seattle; WA
1997-01-01
ALL
Nos 97-2914 to 97-3388 with gaps
Conference paper
English
AIAA , ASME , SAE , ASEE , propulsion
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An Effect of Oxidizer Particle Size on Combustion Stability in Composite Propellants
British Library Conference Proceedings | 2000
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