Development of catalytic materials for decomposition of ADN-based monopropellants

Hydrazine (N2H4), one of the widest used liquid monopropellant is to be replaced by “greener” propellants based on ammonium dinitramide (ADN, NH4+N(NO2)2-), such as LMP-103S and FLP-106 within the framework of the Horizon 2020 Rheform project. While hydrazine can rely on a catalytic technology based...

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Veröffentlicht in:Acta astronautica 2019-05, Vol.158, p.407-415
Hauptverfasser: Maleix, Corentin, Chabernaud, Pierre, Brahmi, Rachid, Beauchet, Romain, Batonneau, Yann, Kappenstein, Charles, Schwentenwein, Martin, Koopmans, Robert-Jan, Schuh, Sebastian, Scharlemann, Carsten
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Sprache:eng
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Zusammenfassung:Hydrazine (N2H4), one of the widest used liquid monopropellant is to be replaced by “greener” propellants based on ammonium dinitramide (ADN, NH4+N(NO2)2-), such as LMP-103S and FLP-106 within the framework of the Horizon 2020 Rheform project. While hydrazine can rely on a catalytic technology based on conventional materials such as γ-Al2O3 (due to the adiabatic decomposition temperature of about 900–1000 °C), LMP-103S and FLP-106 require catalyst support materials that can withstand higher temperatures (about 1650 °C and 1900 °C, respectively) and exhibit a sufficient porosity and resistance to sintering. On these terms, among the various candidates for catalyst support, monolith-shaped supports were investigated. •Ammonium DiNitramide (ADN) investigated in the form of two liquid propellants blends, namely FLP-106 and LMP-103S.•Several catalysts shapes investigated: granulated catalysts and monolithic catalysts.•3D printing of complex ceramic structures investigated towards a washcoating process.•Decomposition tests of FLP-106 and LMP-103S after impregnation of potential active metal solutions.•Textural behaviour of the washcoat layer studied after several heat treatments up to 1500 °C for different durations.
ISSN:0094-5765
1879-2030
DOI:10.1016/j.actaastro.2019.03.033