Recommended Practice for Thrust Measurement in Electric Propulsion Testing

James E. Polk(Jet Propulsion Laboratory), Anthony Pancotti(MSNW (United States)), Thomas Haag(Glenn Research Center), Scott King(Georgia Institute of Technology), Mitchell L. R. Walker(Georgia Institute of Technology), Joseph Blakely(Edwards Air Force Base), John Ziemer(Jet Propulsion Laboratory)
Journal of Propulsion and Power
April 24, 2017
Cited by 125Open Access
Full Text

Abstract

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.


Related Papers