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使用电磁校准技术进行脉冲推力测量。

Pulsed thrust measurements using electromagnetic calibration techniques.

作者信息

Tang Haibin, Shi Chenbo, Zhang Xin'ai, Zhang Zun, Cheng Jiao

机构信息

School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China.

出版信息

Rev Sci Instrum. 2011 Mar;82(3):035118. doi: 10.1063/1.3567803.

Abstract

A thrust stand for accurately measuring impulse bits, which ranged from 10-1000 μN s using a noncontact electromagnetic calibration technique is described. In particular, a permanent magnet structure was designed to produce a uniform magnetic field, and a multiturn coil was made to produce a calibration force less than 10 mN. The electromagnetic calibration force for pulsed thrust measurements was linear to the coil current and changed less than 2.5% when the distance between the coil and magnet changed 6 mm. A pulsed plasma thruster was first tested on the thrust stand, and afterward five single impulse bits were measured to give a 310 μN s average impulse bit. Uncertainty of the measured impulse bit was analyzed to evaluate the quality of the measurement and was found to be 10 μN s with 95% credibility.

摘要

描述了一种用于精确测量脉冲冲量的推力台,其使用非接触式电磁校准技术,脉冲冲量范围为10 - 1000μN·s。具体而言,设计了一种永磁体结构以产生均匀磁场,并制作了一个多匝线圈以产生小于10 mN的校准力。用于脉冲推力测量的电磁校准力与线圈电流呈线性关系,当线圈与磁体之间的距离变化6 mm时,校准力变化小于2.5%。首先在该推力台上对脉冲等离子体推进器进行了测试,随后测量了五个单脉冲冲量,得到平均脉冲冲量为310μN·s。分析了测量脉冲冲量的不确定度以评估测量质量,发现其在95%置信度下为10μN·s。

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