Torsional thrust stand for characterization of microthrusters

This paper describes the setup of a precise thrust stand based on torsional pendulum design for characterizing the performance of microthrusters. Calibration has been carried out by using an improved version of electrostatic calibrator, which produces a wide range of accurate and repeatable calibrat...

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Main Authors: Cheah, K. H., Low, Kay Soon
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2018
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Online Access:https://hdl.handle.net/10356/89855
http://hdl.handle.net/10220/47141
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-898552020-03-07T14:02:36Z Torsional thrust stand for characterization of microthrusters Cheah, K. H. Low, Kay Soon School of Electrical and Electronic Engineering Satellite Research Centre DRNTU::Engineering::Electrical and electronic engineering Thrust Stand Microthrusters This paper describes the setup of a precise thrust stand based on torsional pendulum design for characterizing the performance of microthrusters. Calibration has been carried out by using an improved version of electrostatic calibrator, which produces a wide range of accurate and repeatable calibration force. After the calibration, the thrust stand can resolve constant force from 40μN to 3.4mN and impulse bit from 7μNs to 340μNs. The usefulness of the thrust stand has been demonstrated by measuring the performance of two different microthrusters: a pulsed plasma thruster that produces impulse bit of 23.15μNs and a vaporizing liquid microthruster that produces steady state thrust of 633.5μN. Published version 2018-12-20T09:12:25Z 2019-12-06T17:35:08Z 2018-12-20T09:12:25Z 2019-12-06T17:35:08Z 2016 Journal Article Cheah, K. H., & Low, K. S. (2016). Torsional thrust stand for characterization of microthrusters. IOP Conference Series: Materials Science and Engineering, 152, 012019-. doi:10.1088/1757-899X/152/1/012019 1757-8981 https://hdl.handle.net/10356/89855 http://hdl.handle.net/10220/47141 10.1088/1757-899X/152/1/012019 en IOP Conference Series: Materials Science and Engineering © 2016 The Author(s) (IOP Publishing). Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI. 7 p. application/pdf
institution Nanyang Technological University
building NTU Library
country Singapore
collection DR-NTU
language English
topic DRNTU::Engineering::Electrical and electronic engineering
Thrust Stand
Microthrusters
spellingShingle DRNTU::Engineering::Electrical and electronic engineering
Thrust Stand
Microthrusters
Cheah, K. H.
Low, Kay Soon
Torsional thrust stand for characterization of microthrusters
description This paper describes the setup of a precise thrust stand based on torsional pendulum design for characterizing the performance of microthrusters. Calibration has been carried out by using an improved version of electrostatic calibrator, which produces a wide range of accurate and repeatable calibration force. After the calibration, the thrust stand can resolve constant force from 40μN to 3.4mN and impulse bit from 7μNs to 340μNs. The usefulness of the thrust stand has been demonstrated by measuring the performance of two different microthrusters: a pulsed plasma thruster that produces impulse bit of 23.15μNs and a vaporizing liquid microthruster that produces steady state thrust of 633.5μN.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Cheah, K. H.
Low, Kay Soon
format Article
author Cheah, K. H.
Low, Kay Soon
author_sort Cheah, K. H.
title Torsional thrust stand for characterization of microthrusters
title_short Torsional thrust stand for characterization of microthrusters
title_full Torsional thrust stand for characterization of microthrusters
title_fullStr Torsional thrust stand for characterization of microthrusters
title_full_unstemmed Torsional thrust stand for characterization of microthrusters
title_sort torsional thrust stand for characterization of microthrusters
publishDate 2018
url https://hdl.handle.net/10356/89855
http://hdl.handle.net/10220/47141
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