کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1714645 1519954 2014 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Performance of propellant for ultrasonically aided electric propulsion
ترجمه فارسی عنوان
عملکرد راندمان برای موتور الکتریکی با کمک التراسونیک
کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی


• Description of the UAEP system operation principle.
• Experimental study of the effect of propellant properties on UAEP system.
• Discussion on the effect of propellant properties on UAEP system.
• Choice of the propellant for UAEP system: LiCl/tributyl phosphate.

Ultrasonically aided electric propulsion (UAEP) is a new type of colloid thruster which uses ultrasonic nozzle instead of the traditional capillary or needle emitter. This paper focuses on the effects of propellant upon the performance of UAEP system. Multiple solutions, such as doped formamide, water and tributyl-phosphate were employed and tested as the propellant. The relationships between the spray current and several characteristic parameters of the propellant, such as surface tension coefficient, electrical conductivity, viscosity and doped solute, were experimentally investigated. The experimental results showed that the operation state of UAEP system was greatly influenced by the physical properties of the propellant. The solution of LiCl/tributyl phosphate was selected as the propellant for UAEP.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 98, May–June 2014, Pages 1–8
نویسندگان
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