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タイトルPreliminary Spectroscopic Measurements for a Gallium Electromagnetic (GEM) Thruster
本文(外部サイト)http://hdl.handle.net/2060/20090028644
著者(英)Glumac, Nick G.; Polzin, Kurt A.; Burton, Rodney L.; Thomas, Robert E.
著者所属(英)Illinois Univ. at Urbana-Champaign
発行日2007-07-08
言語eng
内容記述As a propellant option for electromagnetic thrusters, liquid ,gallium appears to have several advantages relative to other propellants. The merits of using gallium in an electromagnetic thruster (EMT) are discussed and estimates of discharge current levels and mass flow rates yielding efficient operation are given. The gallium atomic weight of 70 predicts high efficiency in the 1500-2000 s specific impulse range, making it ideal for higher-thrust, near-Earth missions. A spatially and temporally broad spectroscopic survey in the 220-520 nm range is used to determine which species are present in the plasma and estimate electron temperature. The spectra show that neutral, singly, and doubly ionized gallium species are present in a 20 J, 1.8 kA (peak) are discharge. With graphite present on the insulator to facilitate breakdown, singly and doubly ionized carbon atoms are also present, and emission is observed from molecular carbon (CZ) radicals. A determination of the electron temperature was attempted using relative emission line data, and while the spatially and temporally averaged, spectra don't fit well to single temperatures, the data and presence of doubly ionized gallium are consistent with distributions in the 1-3 eV range.
NASA分類Propellants and Fuels
レポートNOMSFC-302
AIAA Paper 2007-5855
権利Copyright, Distribution as joint owner in the copyright


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