Thrust Measurement of an Integrated Multi-Sensor Micro-Newton Cold Gas Thruster
In recent years, cold gas thrusters have been successfully deployed in numerous missions, showcasing their exceptional reliability and enabling ultra-precise space operations across a broad thrust range. This article introduces an integrated cold gas thruster that integrates flow, pressure, and displacement sensors. The thrust range of this thruster can exceed 1000 μN at most, and the resolution can reach up to 0.1 μN at low thrust. The results of the high-precision displacement sensor are good, showing that the thruster performs well in terms of flow control accuracy and thrust output sensitivity. The measurement accuracy of the force frame itself is also excellent, and it can detect small thrust changes of 0.1 μN. The thrust noise level of the thruster is good, comparable to the standard noise levels of the experimental environment.
Authors
- Yong Gao
- Gang Meng (ORCID: https://orcid.org/0000-0002-3365-8963)
- Jun Long (ORCID: https://orcid.org/0000-0003-0163-0007)
- Haibo Tu (ORCID: https://orcid.org/0000-0002-3521-7264)
- Xinju Fu
- Xudong Wang (ORCID: https://orcid.org/0000-0001-6435-5247)
- Xuhui Liu (ORCID: https://orcid.org/0000-0001-6929-4500)
- Yong Li (ORCID: https://orcid.org/0000-0003-2278-6991)
- Songcai Lu
Institutions
- Chinese Academy of Sciences (CN)
- Institute of Geodesy and Geophysics (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-03-06
- DOI
- https://doi.org/10.3390/aerospace12030210
- Primary Topic
- Plasma Diagnostics and Applications
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- National Natural Science Foundation of China
- National Key Research and Development Program of China