Nano‐Computed Tomographic Measurements of Partially Decomposed Ammonium Perchlorate Particles

High performance solid rocket motors typically contain ammonium perchlorate (AP) particles as the oxidizer. Ammonium perchlorate provides good performance, but thermal decomposition leads to safety concerns for handling and storing solid propellant. Computed tomography is shown to allow for visualiz...

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Veröffentlicht in:	Propellants, explosives, pyrotechnics explosives, pyrotechnics, 2017-09, Vol.42 (9), p.1111-1116
Hauptverfasser:	Kalman, Joseph, Hedman, Trevor, Varghese, Bino, Dagliyan, Grant
Format:	Artikel
Sprache:	eng
Schlagworte:	ammonium perchlorate Computation Computed tomography Decomposition Environmental testing Heating insensitive munition Motors Particle size distribution Pore size distribution Porosity propellants Rocket engines Rockets Solid propellant rocket engines Solid propellants Thermal decomposition
Online-Zugang:	Volltext
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