2013
DOI: 10.1109/tmech.2013.2249085
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A MEMS-Based Catalytic Microreactor for a H$_{\bf 2}$O$_{\bf 2}$ Monopropellant Micropropulsion System

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Cited by 25 publications
(17 citation statements)
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“…Here, A 0 is the pre‐exponential or frequency factor, E a is the activation energy of the decomposition reaction, R is the universal gas constant (8.314 J (mol·K) −1 ) and T is the temperature of the system in K. A 0 indicates the total number of collisions in a reaction, which is usually temperature‐dependent and must be experimentally determined . For a catalytic decomposition reaction, other authors even stated that the value of A 0 is dependent on the surface‐to‐volume ratio of the catalyst . Finally, Zhou and Hitt analytically determined the reaction kinetics for the catalytic decomposing reaction of H 2 O 2 gas on an iron catalyst to be A 0 = 10 9 s −1 and E a = 50.2 kJ mol −1 .…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Here, A 0 is the pre‐exponential or frequency factor, E a is the activation energy of the decomposition reaction, R is the universal gas constant (8.314 J (mol·K) −1 ) and T is the temperature of the system in K. A 0 indicates the total number of collisions in a reaction, which is usually temperature‐dependent and must be experimentally determined . For a catalytic decomposition reaction, other authors even stated that the value of A 0 is dependent on the surface‐to‐volume ratio of the catalyst . Finally, Zhou and Hitt analytically determined the reaction kinetics for the catalytic decomposing reaction of H 2 O 2 gas on an iron catalyst to be A 0 = 10 9 s −1 and E a = 50.2 kJ mol −1 .…”
Section: Introductionmentioning
confidence: 99%
“…A two‐dimensional (2D) model of a H 2 O 2 micro‐thruster assembly, where rhodium dioxide (RhO2) nano‐rods were used as a catalyst, was studied by Widdis et al . In their work, the porosity and surface effects of the catalytic surface were not considered.…”
Section: Introductionmentioning
confidence: 99%
“…In this investigation, the same RuO 2 NR coating was used to enhance the reactivity of two different chemical reaction systems. In the first case, the walls of a micro-reactor were coated with a RuO 2 NR film, for the purpose of enhancing the decomposition of a high concentration (30%) H 2 O 2 monopropellant fuel for implementation in a micropropulsion system for small satellites [1] [2]. In the second reaction system, the RuO 2 NR coating was applied to the surface of a conductive electrode that was used to electrolyze an aqueous solution of H 2 SO 4 [3].…”
Section: Introductionmentioning
confidence: 99%
“…Several H 2 O 2 propulsion concepts have been under investigation by different groups, including monopropellant [3][4][5][6][7][8], bipropellant [1,[9][10][11][12][13], and hybrid systems [14,15]. The former two primarily address low-to-medium thrust ranges and are therefore mostly used for attitude control applications.…”
Section: Introductionmentioning
confidence: 99%