Electric-propulsion-field microthrust transient measurement system based on dynamic photoelastic method
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- NAT UNIV OF DEFENSE TECH
- Publication Date
- 2017-11-07
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Abstract
Description
technical field
[0001] The invention relates to a micro-thrust measurement system, in particular to a real-time measurement system for the micro-thrust in the field of electric propulsion. Background technique
[0002] At present, the domestic high-precision measurement of micro-thrust and micro-impulse of electric propulsion thrusters is more commonly based on thrust measurement systems such as simple pendulum, inverted pendulum, and torsion pendulum. Among them, when the electromagnetic balance based on the inverted pendulum principle measures the impulse, there is a serious zero point drift, and the unstable balance position of the electromagnetic balance also leads to poor measurement accuracy. Therefore, it can generally only be used for qualitative or semi-quantitative analysis.
[0003] Relatively speaking, the use of torsion pendulum to measure thrust or impulse has high accuracy and sensitivity. The history of torsion pendulum can be traced back to the torsion balan...