کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1690272 1518984 2006 5 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Effect of solute mixing in the liquid propellant of a pulsed plasma thruster
موضوعات مرتبط
مهندسی و علوم پایه مهندسی مواد سطوح، پوشش‌ها و فیلم‌ها
پیش نمایش صفحه اول مقاله
Effect of solute mixing in the liquid propellant of a pulsed plasma thruster
چکیده انگلیسی

Sodium chloride or ammonia was dissolved in the water propellant of pulsed plasma thrusters to improve the performance. Pulsed plasma thrusters using liquid propellant utilize water as attractive alternative instead of Teflon. Water propellant enables in controlling propellant mass flow and leads to high specific impulse. However, liquid propellant pulsed plasma thrusters have larger plasma resistance and lower thrust power ratio than the common Teflon propellant thruster. Here, sodium chloride and ammonia solution of water were examined to decrease that plasma resistance. As a result, emission lines attributed from the solute were observed using sodium chloride aqueous solution propellant, and a 5% reduction of the plasma resistance was shown, and the thrust to power was increased. However, ammonia aqueous solution decreased the thruster performance.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Vacuum - Volume 80, Issues 11–12, 7 September 2006, Pages 1234–1238
نویسندگان
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