2012
DOI: 10.1016/j.apcatb.2012.08.009
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HAN and ADN as liquid ionic monopropellants: Thermal and catalytic decomposition processes

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Cited by 79 publications
(24 citation statements)
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“…The introduction of hydroxylammonium nitrate (HAN) ionic liquid as a replacement for hydrazine as a spacecraft monopropellant has been of great interest recently due to the reduced toxicity and the improved performance afforded by HAN over hydrazine. HAN is one component of the formulation used in the small demonstration satellite-4 (SDS-4) developed by the Japan Aerospace Exploration Agency, and it is a component of the AF-M315E monopropellant to be used in NASA’s Green Propellant Infusion Mission. , Extensive experimental work has been performed on the thermal decomposition of HAN by Cronin and Brill, Oxley and Brower, Lee and Litzinger, and Kappenstein et al While much effort has been dedicated to understanding the HAN thermal decomposition mechanism (over 30 publications), only very recently have efforts been made to understand the catalytic decomposition mechanism of HAN in order to optimize the design of HAN-based monopropellant catalysts and thrusters. , A brief summary of the HAN thermal decomposition mechanism is presented here. A detailed overview of the current understanding of both thermal decomposition and catalytic decomposition of HAN can be found elsewhere (in ref and references therein).…”
mentioning
confidence: 99%
“…The introduction of hydroxylammonium nitrate (HAN) ionic liquid as a replacement for hydrazine as a spacecraft monopropellant has been of great interest recently due to the reduced toxicity and the improved performance afforded by HAN over hydrazine. HAN is one component of the formulation used in the small demonstration satellite-4 (SDS-4) developed by the Japan Aerospace Exploration Agency, and it is a component of the AF-M315E monopropellant to be used in NASA’s Green Propellant Infusion Mission. , Extensive experimental work has been performed on the thermal decomposition of HAN by Cronin and Brill, Oxley and Brower, Lee and Litzinger, and Kappenstein et al While much effort has been dedicated to understanding the HAN thermal decomposition mechanism (over 30 publications), only very recently have efforts been made to understand the catalytic decomposition mechanism of HAN in order to optimize the design of HAN-based monopropellant catalysts and thrusters. , A brief summary of the HAN thermal decomposition mechanism is presented here. A detailed overview of the current understanding of both thermal decomposition and catalytic decomposition of HAN can be found elsewhere (in ref and references therein).…”
mentioning
confidence: 99%
“…The subsequent decomposition is a two-step exothermic process. 13,18 Decomposition onset temperatures for HAN have been reported in the range of 100−140°C. (1)…”
mentioning
confidence: 99%
“…But, the decomposition of HAN/AC-RF mixture with is occurred with exotherm of two peaks at 209 and 288 °C. This phenomenon has been noted in the previous studies [1,2,17] concerning the decomposition of HAN without any additives, where a two-stage mechanism for decomposition of the mixture is proposed. Thus, we guess that activated carbon AC-RF, does not change the decomposition mechanism of HAN.…”
Section: Han + Hmentioning
confidence: 83%
“…Therefore, by the end of the twentieth century, the research centers have an intention on searching of new less harmful and higher-energy materials. Aqueous compounds such as hydroxymammonium nitrate (NH 3 OHNO 3 ) were proposed as one of the most promising alternative for hydrazine [1][2].…”
Section: Introductionmentioning
confidence: 99%