5 N Scale Preliminary Thruster Test with an ADN-based monopropellant 5 N 급 ADN 기반 단일추진제 추력기 예비 연소 시험

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This paper reports the preliminary firing test performed with an ADN-based monopropellant using a 5 N scale thruster. ADN-based propellant and catalyst was fabricated and catalytic combustion of propellant was characterized by DSC-TG analysis. Although an explosion in the catalyst bed was occurred, high temperature in the catalyst bed obtained and demonstrated catalytic combustion of the propellant. Preliminary test results motivates the research for catalysts with better thermal stability
Publisher
한국추진공학회
Issue Date
2018-04
Language
English
Keywords

암모늄 디나이트라마이드; 촉매 점화; 단일추진제 추력기; 란타늄 헥사알루미네이트; Ammonium Dinitramide; Catalytic Ignition; Monopropellant Thruster; Lanthanum Hexaaluminate

Citation

한국추진공학회지, v.22, no.2, pp.29 - 37

ISSN
1226-6027
DOI
10.6108/KSPE.2018.22.2.029
URI
http://hdl.handle.net/10203/244586
Appears in Collection
AE-Journal Papers(저널논문)
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