Thermal Decomposition Kinetics Studies of Ammonium Perchlorate - HTPB /Al/AP Solid Propellants formulated with Iron Oxide burning rate catalyst in Nano and Micro scale
Author:
Affiliation:
1. Avibrás Aerospace Industry
2. Aeronautical Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4088
Reference25 articles.
1. 1Prajakta, R.P., Krishnamurthy, V.N., Satyawati, S.J., 2006, "Differential Scanning Calorimetric Study of HTPB based Composite PropellantsinPresence ofNano Ferric Oxide", PropellantsExplosives, PyrotechnicsVol. 31, No6,pp. 442-446.
2. Propelente sólido compósito polibutadiênico: I- influência do agente de ligação
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