Isolating the effects of oxidizer characteristics and catalytic additives on the high-pressure exponent break of AP/HTPB-Composite propellants
Author:
Funder
Turbomachinery Laboratory
Publisher
Elsevier BV
Subject
Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering
Reference27 articles.
1. Deflagration characteristics of ammonium perchlorate at high pressures
2. A study of the ethylene oxide decomposition flame
3. Further studies of pure ammonium perchlorate deflagration
4. Le transfert de modulation des objectifs
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2. Prediction of Solid Propellant Burning Rate Characteristics Using Machine Learning Techniques;Propellants, Explosives, Pyrotechnics;2023-03-16
3. Facile fabrication and catalytic activity of nickel to ferric oxide nanoparticles for ammonium perchlorate decomposition;Brazilian Journal of Chemical Engineering;2023-01-18
4. Combustion behavior and mechanism of molecular perovskite energetic material DAP-4-based composites with metal fuel Al;Defence Technology;2022-11
5. High-Pressure Combustion Characteristics of Hydroxyl-Terminated Polybutadiene Propellants;Journal of Propulsion and Power;2022-10-07
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