Research Progress on Micro-thrust and Micro-impulse Measurement Technology of PPT

被引：2

作者：

Du, Xinru ^{[1
]}

Wu, Jianjun ^{[1
]}

Zhang, Yu ^{[1
]}

Li, Jian ^{[1
]}

Tan, Sheng ^{[1
]}

Ou, Yang ^{[1
]}

机构：

[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China

来源：

4TH INTERNATIONAL CONFERENCE ON ENERGY SCIENCE AND APPLIED TECHNOLOGY (ESAT 2018) | 2019年 / 2066卷

关键词：

PPT; Micro-Thrust; Micro-Impulse; Measurement System; STAND; BALANCE;

D O I：

10.1063/1.5089044

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

The pulsed plasma thruster (PPT) is a potential electric thruster for microsatellites. One important content of PPT performance research is the measurement of micro-thrust and micro-impulse. This paper summarizes the 4 typical dynamic measuring systems at home and abroad, which include the single pendulum type, the torsion pendulum type, the cantilever type and the balance type. In the paper, the structure principle, measurement performance, advantages and disadvantages of various configurations are compared and analyzed. The development process of each micro-thrust and micro-impulse measurement technology is summarized, and its developing trend is prospected.

引用

页数：10

共 23 条

[1]

Andrew Cubbin Edward, 1998, THRUST MEASUREMENT U

[2]

Cubbin E. A., 1996, PULSED THRUST MEASUR

[3] Pulsed thrust measurements using laser interferometry [J].

Cubbin, EA ;

Ziemer, JK ;

Choueiri, EY ;

Jahn, RG .

REVIEW OF SCIENTIFIC INSTRUMENTS, 1997, 68 (06) :2339-2346

[4] Investigation of time-dependent forces on a nano-Newton-second impulse balance [J].

D'Souza, BC ;

Ketsdever, AD .

REVIEW OF SCIENTIFIC INSTRUMENTS, 2005, 76 (01)

[5]

Emhoff J. M., 2007, AIAA20075299

[6] Measurement of Newton's constant using a torsion balance with angular acceleration feedback [J].

Gundlach, JH ;

Merkowitz, SM .

PHYSICAL REVIEW LETTERS, 2000, 85 (14) :2869-2872

[7] Precision electromagnetic calibration technique for micro-Newton thrust stands [J].

He, Zhen ;

Wu, Jianjun ;

Zhang, Daixian ;

Lu, Gaofei ;

Liu, Zejun ;

Zhang, Rui .

REVIEW OF SCIENTIFIC INSTRUMENTS, 2013, 84 (05)

[8]

[侯大立 HOU Dali], 2008, [推进技术, Journal of Propulsion Technology], V29, P377

[9]

Hu Zongsen, 2002, RES PERFORMANCE PULS

[10] Development of thrust stand for low impulse measurement from microthrusters [J].

Koizumi, H ;

Komurasaki, K ;

Arakawa, Y .

REVIEW OF SCIENTIFIC INSTRUMENTS, 2004, 75 (10) :3185-3190

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