Article ID Journal Published Year Pages File Type
40494 Applied Catalysis A: General 2013 5 Pages PDF
Abstract

The catalytic performance of Ir-based catalyst for the decomposition of high energetic liquid propellant was investigated in a monopropellant thruster. The changes of ignition delay, catalyst bed temperature and chamber pressure with the numbers of pulse-injection were demonstrated to be effective signposts of catalyst bed efficiencies. The catalyst in fresh state and that after its deactivation were characterized by N2-physisorption, XRD, H2-chemisorption, TEM, H2-TPR and XPS. It was noted that the particle distribution and oxidation state of iridium are the major indicators of catalyst deactivation.

Graphical abstractFigure optionsDownload full-size imageDownload high-quality image (313 K)Download as PowerPoint slideHighlights► Uniform distribution of nano-size iridium particles into the alumina before test. ► Deactivation of iridium catalyst after HAN decomposition. ► Deactivation phenomena was caused by oxidation of iridium. ► Severe sintering of iridium catalyst after HAN decomposition reaction.

Related Topics
Physical Sciences and Engineering Chemical Engineering Catalysis
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