Experimental investigation of the catalytic decomposition and combustion characteristics of a non-toxic ammonium dinitramide (ADN)-based monopropellant thruster. (December 2016)

• Record Type: Journal Article
• Authors: Chen, Jun; Li, Guoxiu; Zhang, Tao; Wang, Meng; Yu, Yusong
• Is Part Of: Acta astronautica. Volume 129(2016)
• Page Start: 367
• Page End: 373
• Publication Date: 2016-12
• Subjects: Experimental investigation -- Catalytic decomposition and combustion -- Non-toxic -- Ammonium dinitramide -- Preheating temperature -- Feed pressure; Astronautics -- Periodicals; Outer space -- Exploration -- Periodicals; Astronautics; Periodicals; 629.405
• DOI: 10.1016/j.actaastro.2016.09.027
• Languages: English
• ISSNs: 0094-5765

Abstract

Abstract: Low toxicity ammonium dinitramide (ADN)-based aerospace propulsion systems currently show promise with regard to applications such as controlling satellite attitude. In the present work, the decomposition and combustion processes of an ADN-based monopropellant thruster were systematically studied, using a thermally stable catalyst to promote the decomposition reaction. The performance of the ADN propulsion system was investigated using a ground test system under vacuum, and the physical properties of the ADN-based propellant were also examined. Using this system, the effects of the preheating temperature and feed pressure on the combustion characteristics and thruster performance during steady state operation were observed. The results indicate that the propellant and catalyst employed during this work, as well as the design and manufacture of the thruster, met performance requirements. Moreover, the 1 N ADN thruster generated a specific impulse of 223 s, demonstrating the efficacy of the new catalyst. The thruster operational parameters (specifically, the preheating temperature and feed pressure) were found to have a significant effect on the decomposition and combustion processes within the thruster, and the performance of the thruster was demonstrated to improve at higher feed pressures and elevated preheating temperatures. A lower temperature of 140 °C was determined to activate the catalytic decomposition and combustion processes more effectively compared with the results obtained using other conditions. The data obtained in this study should be beneficial to future systematic and in-depth investigations of the combustion mechanism and characteristics within an ADN thruster. Highlights: The decomposition and combustion process is investigated by experimental method. The effects brought by diverse feed pressure and preheating temperature are studied. An optimized combustion chamber temperature is achieved under diverse feed pressure. A lower temperature can activate the catalytic decomposition and combustion processes.