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Spectroscopic and Electrostatic Investigation of the Diverging Cusped-Field Thruster
2009
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
unpublished
A magnetized plasma thruster variant with a divergent chamber and strong magnetic cusps has been been prototyped and preliminarily characterized at the MIT Space Propulsion Laboratory. This paper expands upon the previous work with a non-invasive, optical examination of the near-field plume and discharge chamber phenomena. Calibrated broadband spectra reveal changes in Xe I and II level populations with operational mode, while high resolution narrow bandwidth scans are used to examine trends in
doi:10.2514/6.2009-4813
fatcat:rgnsyudqv5efbk6347c4dfduje