Proceedings of the 2016 7th International Conference on Mechatronics, Control and Materials (ICMCM 2016)

The measurement of low impulse from pulsed electromagnetic thrusters by thrust stand

Authors
Chenyang Ding, Mousen Cheng
Corresponding Author
Chenyang Ding
Available Online December 2016.
DOI
10.2991/icmcm-16.2016.23How to use a DOI?
Keywords
Low impulse measurement; thrust stand; pulsed electromagnetic thruster.
Abstract

Two types of measurement methods are given to determine the low impulse involved in the working process of pulsed electromagnetic plasma thrusters. Different mechanical devices, including pendulum and critical stress thrust stands, are introduced and compared with others concomitant with respective typical applications. Advantages as well as disadvantages of these thrust stands are discussed, which can provide a favorable reference for pulsed electromagnetic plasma thrusters' micro-impulse measurement and research.

Copyright
© 2016, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 2016 7th International Conference on Mechatronics, Control and Materials (ICMCM 2016)
Series
Advances in Engineering Research
Publication Date
December 2016
ISBN
10.2991/icmcm-16.2016.23
ISSN
2352-5401
DOI
10.2991/icmcm-16.2016.23How to use a DOI?
Copyright
© 2016, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Chenyang Ding
AU  - Mousen Cheng
PY  - 2016/12
DA  - 2016/12
TI  - The measurement of low impulse from pulsed electromagnetic thrusters by thrust stand
BT  - Proceedings of the 2016 7th International Conference on Mechatronics, Control and Materials (ICMCM 2016)
PB  - Atlantis Press
SP  - 112
EP  - 116
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmcm-16.2016.23
DO  - 10.2991/icmcm-16.2016.23
ID  - Ding2016/12
ER  -