Development and tests of a thrust stand with an in-situ null position adjustment and calibration method for low power plasma thrusters-Reference-Cited by-同舟云学术

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Development and tests of a thrust stand with an in-situ null position adjustment and calibration method for low power plasma thrusters

Published:2023-06 Issue: Volume:18 Page:101219
ISSN:2590-1230
Container-title:Results in Engineering
language:en
Short-container-title:Results in Engineering

Author:

Kokal Ugur,Saridede Emin^ORCID,Celik Murat^ORCID

Funder

TÜBİTAK

Boğaziçi University

Publisher

Elsevier BV

Subject

General Engineering

Reference27 articles.

1. Performance evaluation of spacecraft propulsion systems in relation to mission impulse requirements;Erichsen,1997

2. Encyclopedia of Physical Science and Technology, vol. 3;Jahn,2002

3. Development of a mili-Newton level thrust stand for thrust measurements of electric propulsion systems and UK90 Hall effect thruster;Kokal,2018

4. Development of a highly precise micro-Newton thrust balance;Hey;IEEE Trans. Plasma Sci.,2014

5. Recommended practices in thrust measurements;Polk,2013

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