Theoretical investigation of the catalytic effect of microingredients on ammonium perchlorate (AP) thermal decomposition
Author:
Affiliation:
1. Department of Chemical and Materials Engineering, Chung Cheng Institute of TechnologyNational Defense University Ta‐Hsi Tao‐Yuan Taiwan, R.O.C.
Publisher
Wiley
Subject
General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/jccs.201800195
Reference38 articles.
1. Test-Based Thermal Decomposition Simulation of AP/HTPB and AP/HTPE Propellants
2. R.Behrens L.Minier 33rd JANNAF Combustion Subcommittee Meeting1996 report No. 14.
3. Study on the Burning Characteristics of AP/Al/HTPB Composite Solid Propellant Containing Nano-Sized Ferric Oxide Powder
4. Thermal Decomposition Behaviors and Burning Characteristics of Composite Propellants Prepared Using Combined Ammonium Perchlorate/Ammonium Nitrate Particles
5. Recent advances in new oxidizers for solid rocket propulsion
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