Recommended Practice for Thrust Measurement in Electric Propulsion Testing

被引:79
|
作者
Polk, James E. [1 ]
Pancotti, Anthony [2 ]
Haag, Thomas [3 ]
King, Scott [4 ]
Walker, Mitchell [4 ]
Blakely, Joseph [5 ]
Ziemer, John [6 ]
机构
[1] CALTECH, Jet Prop Lab, Prop Thermal & Mat Engn Sect, M-S 125-109,4800 Oak Grove Drive, Pasadena, CA 91109 USA
[2] MSNW LLC, Redmond, WA 98052 USA
[3] NASA, John H Glenn Res Ctr, Space Prop Branch, Cleveland, OH 44135 USA
[4] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA 30332 USA
[5] ERC Inc, Edwards AFB, CA 93523 USA
[6] CALTECH, Jet Prop Lab, JPL Innovat Foundry, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
关键词
BALANCE; STAND; CALIBRATION;
D O I
10.2514/1.B35564
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The accurate, direct measurement of thrust or impulse is one of the most critical elements of electric thruster characterization, and it is one of the most difficult measurements to make. This paper summarizes recommended practices for the design, calibration, and operation of pendulum thrust stands, which are widely recognized as the best approach for measuring micronewton- to millinewton-level thrust and micronewton-per-second-level impulse bits. The fundamentals of pendulum thrust stand operation are reviewed, along with the implementation of hanging pendulum, inverted pendulum, and torsional balance configurations. The methods of calibration and recommendations for calibration processes are presented. Sources of error are identified, and methods for data processing and uncertainty analysis are discussed. This review is intended to be the first step toward a recommended practices document to help the community produce high-quality thrust measurements.
引用
收藏
页码:539 / 555
页数:17
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