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
01.01.2002
17 pages
Aufsatz (Konferenz)
Englisch
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AIAA | 1981
|Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure
Online Contents | 2017
|AIAA | 2005
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