Siberian Federal University

Issue

Journal of Siberian Federal University. Engineering & Technologies. 2024 17 (4)

Authors

Vavilov, Igor S.; Lokotaev, Dmitry V.; Yachmenev, Pavel S.; Fedyanin, Victor V.; Zharikov, Konstantin I.; Stepen, Pavel V.; Lukyanchik, Anton I.

Contact information

Vavilov, Igor S.: Omsk State Technical University Omsk, Russian Federation; ; Lokotaev, Dmitry V.: Omsk State Technical University Omsk, Russian Federation; Yachmenev, Pavel S.: Omsk State Technical University Omsk, Russian Federation; Fedyanin, Victor V.: Omsk State Technical University Omsk, Russian Federation; Zharikov, Konstantin I.: Omsk State Technical University Omsk, Russian Federation; Stepen, Pavel V.: Omsk State Technical University Omsk, Russian Federation; Lukyanchik, Anton I.: Omsk State Technical University Omsk, Russian Federation

Keywords

LVDS; swing stand; target; disk; membrane; optical sensor; jet propulsion; ion thruster; calibration; LVDS; capacitive sensor; interferometer

Abstract

The paper provides an overview of most existing designs of power stand based on a swing and an elastic target designed to measure the thrust of ion thruster. There are 7 unique design of a swing stands and 16 designs of aerodynamic stands based on an elastic target. The presented a swing stands cover the range of steady-state thrust from 50 μN to 1500 μN and thrust pulses in the range from 1 μN · s to 150 mN·s. Stands based on elastic targets cover the range of steady-state thrust from 3 μN to 1 N. The time period from 1972 to 2023 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 measuring thrust by stands are presented

Pages

474–504

EDN

RCHUHW

Paper at repository of SibFU

https://elib.sfu-kras.ru/handle/2311/153187

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).