کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5028780 1470641 2017 7 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Development of KM-60 Based Orbit Control Propulsion Subsystem for Geostationary Satellite
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی (عمومی)
پیش نمایش صفحه اول مقاله
Development of KM-60 Based Orbit Control Propulsion Subsystem for Geostationary Satellite
چکیده انگلیسی

The paper contains the development results of an orbit-control electric jet propulsion subsystem intended for a geostationary satellite based on the EXPRESS-1000 family medium class platform. The subsystem is based on the newly-developed KM-60 thrusters featuring an increased specific pulse, and equipped with a Xenon storage tank made of composites, a small-sized Xenon feed unit, PPU and dedicated software. During the development stage, scientific and technical tasks were carried out to ensure thruster performance stability over the lifetime, to create a power processing system featuring increased output voltage, and a control unit operating through a multiplex data bus. As a result, a thruster subsystem significantly exceeding similar subsystems in main parameters was developed and implemented.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Procedia Engineering - Volume 185, 2017, Pages 319-325
نویسندگان
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