4.4 Article

Burning Rate Characterization of Ammonium Perchlorate Pellets Containing Micro- and Nano-Catalytic Additives

Journal

JOURNAL OF PROPULSION AND POWER
Volume 38, Issue 5, Pages 822-832

Publisher

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.B38635

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Ammonium perchlorate (AP) is a commonly used oxidizer in composite propellants, and its combustion behavior can be controlled by micro- and nano-metal oxide catalysts. The study found that micro-iron oxide increased the burning rate of AP within a certain pressure range, while nano-titanium oxide and nano-iron oxide increased the burning rate at higher pressures. The presence of catalytic additives eliminated the negative slope typically observed in the burning rate curve of plain AP, and nano-additive formulations showed higher low-pressure deflagration limits.
Ammonium perchlorate (AP) is a common oxidizer in composite propellants, and its combustion behavior can be tailored by micro- and nano-metal oxide catalysts. Ammonium perchlorate pellets were manufactured with micro- and nano-titanium oxide (TiO2) and iron oxide (Fe2O3) at several mass loadings (0-3%) to isolate their effects on AP. The samples were burned from 3.45 to 34.5 MPa (500-5000 psi) in a constant-volume strand bomb. Microscopy characterization was completed for both additives and representative pellets. The incorporation of 1% micro-Fe2O3 yielded the highest burning rate within the investigated pressure range. All micro-additive formulations increased the burning rate at pressures ranging from roughly 13.45 to 17.24 MPa (1950-2500 psi) and from 4.50 to 8.60 MPa (650-1250 psi) for micro-TiO2 and micro-Fe2O3, respectively, and these effects were dependent on catalyst mass loading. The burning rates were increased at pressures greater than 11.27 (1620 psi) and 8.27 MPa (1200 psi) for nano-TiO2 and nano-Fe2O3, respectively. Both nano-additives yielded burning rates that were independent of mass loading within the range of evaluated concentrations (0.25-1%). In all cases, the presence of the catalytic additives removed the negative slope generally observed in the burning rate curve of plain AP. Higher low-pressure deflagration limits were observed for nano-additive formulations, potentially due to radiative heat losses.

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