A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

Qiang Shen; Weizheng Yuan; Jianbing Xie; Honglong Chang

doi:10.1007/s00542-015-2486-7

A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

Qiang Shen, Weizheng Yuan, Jianbing Xie, Honglong Chang

School of Mechanical Engineering

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

8 Scopus citations

Abstract

This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.

Original language	English
Pages (from-to)	847-859
Number of pages	13
Journal	Microsystem Technologies
Volume	22
Issue number	4
DOIs	https://doi.org/10.1007/s00542-015-2486-7
State	Published - 1 Apr 2016

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title = "A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification",

abstract = "This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.",

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AU - Chang, Honglong

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Y1 - 2016/4/1

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AB - This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.

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A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

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