Dynamic-force extraction for micro-propulsion testing: Theory and experimental validation-Reference-Cited by-同舟云学术

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Dynamic-force extraction for micro-propulsion testing: Theory and experimental validation

Published:2018-11 Issue:11 Volume:89 Page:115110
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Review of Scientific Instruments

Author:

Wang Chuansheng¹²,Guan Changbin³,Liu Xuhui³,Wang Xudong³,Li Fei¹^ORCID,Yu Xilong¹²

Affiliation:

1. State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, CAS, Beijing 100190, China

2. School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China

3. Beijing Institute of Control Engineering, China Academy of Space Technology, Beijing 100190, China

Funder

the scientific instrument developing project of the chinese academy of sciences

Youth Innovation Promotion Association of the Chinese Academy of Sciences

Publisher

AIP Publishing

Subject

Instrumentation

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5037365

Reference24 articles.

1. Gas Dynamic Calibration of a Nano-Newton Thrust Stand

2. Development of thrust stand for low impulse measurement from microthrusters

3. Design and characterization of a nano-Newton resolution thrust stand

4. A torsional balance for the characterization of microNewton thrusters

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Study of the thrust response characteristics of Hall Micro Thruster;Results in Physics;2024-02

2. Experimental study on the response time of microthrust;Acta Mechanica Sinica;2023-06-20

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