Propellants and explosives : thermochemical aspects of combustion

By 浪之介久保田. 2007

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Modeling of combustion and ignition of solid-propellant ingredients (2007, background): “The most commonly employed binders are either inert (typically HTPB, hydroxyl-terminated polybutadiene, with various plasticizers, ballistic modifiers, and crosslinking agents), or active (NG and NC, polyether polymer, and azide polymer such as GAP glycidyl azide polymer, BAMO bis-azidomethyl oxetan”
Stabilizers for nitrate ester-based energetic materials and their mechanism of action: a state-of-the-art review (2017, background): “[4] Kubota N (2015) Propellants and explosives: thermo-”
Synthesis, Characterization and Applications of Iron Oxide Nanoparticles - a Short Review (2015, background): “Moreover, one of the most important parameters to characterize the performance of composite solid propellants is the burning rate which is function of the internal pression of combustion chamber, usually expressed by the following empirical equation V = a x P n (Kubota 2007), where V is the burning ”