Overview of known power methods for measuring the jet thrust of ion engines: vertical pendulums
Автор: Vavilov I.S., Lokotaev D.V., Yachmenev P.S., Fedyanin V.V., Zharikov K.I., Stepen P.V., Lukyanchik A.I.
Журнал: Журнал Сибирского федерального университета. Серия: Техника и технологии @technologies-sfu
Рубрика: Исследования. Проектирование. Опыт эксплуатации
Статья в выпуске: 3 т.17, 2024 года.
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The paper presents an overview of the majority of existing designs of power stands based on a vertical pendulum designed to measure the thrust of ion thruster. 22 unique stand designs developed by various scientific groups are presented. The presented stands cover the range of steady-state loads of 1 nN to 5 N and thrust pulses in the range from 200 µN · s to 800 µN ·s. The temporary section from 1991 to 2022 is covered. The methods of recording micro displacement of the sensing element, damping of parasitic vibrations and calibration of stands are shown. Data on errors in the measurement of traction by stands are presented.
Vertical pendulum, inverted pendulum, optical sensor, jet propulsion, ion thruster, calibration, lvds, capacitive sensor, interferometer
Короткий адрес: https://sciup.org/146282876
IDR: 146282876