Molybdenum Trioxide effects on HTPB/AP/A1 Based Propellant Burning Rate
8th, International workshop on combustion and propulsion; Rocket propulsion present and future ; 2002 ; Possuoli, Italy
2002-01-01
17 pages
Conference paper
English
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Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure
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