@inproceedings{e6ac7c5e747a4f43957df63e374546c7,
title = "Optimization of the AF-MPDT geometry and operating parameters for the low current to mass flow rate ratio regime",
abstract = "The theoretical, experimental and numerical investigation have been performed in order to obtain the guidelines for the design and operating parameters envelope optimization of the AF-MPDT operating in low discharge current high mass flow rate regime. The power range of the target thruster is 5-10 kW, current levels are 100-180 A, total mass flow rate is 21 mg/s, maximal applied magnetic field strength 0.133 T. At the current stage of the research the maximal thrust efficiency obtained is 21\%, the maximal thrust-296 mN. The suggestions for the further thruster optimization are presented.",
author = "Alena Kitaeva and Haibin Tang and Baojun Wang and Tommaso Andreussi",
note = "Publisher Copyright: {\textcopyright} 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 49th AIAA Plasmadynamics and Lasers Conference, 2018 ; Conference date: 25-06-2018 Through 29-06-2018",
year = "2018",
doi = "10.2514/6.2018-3266",
language = "英语",
isbn = "9781624105494",
series = "2018 Plasmadynamics and Lasers Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "2018 Plasmadynamics and Lasers Conference",
}