Literature DB >> 19485530

High-power, null-type, inverted pendulum thrust stand.

Kunning G Xu1, Mitchell L R Walker.   

Abstract

This article presents the theory and operation of a null-type, inverted pendulum thrust stand. The thrust stand design supports thrusters having a total mass up to 250 kg and measures thrust over a range of 1 mN to 5 N. The design uses a conventional inverted pendulum to increase sensitivity, coupled with a null-type feature to eliminate thrust alignment error due to deflection of thrust. The thrust stand position serves as the input to the null-circuit feedback control system and the output is the current to an electromagnetic actuator. Mechanical oscillations are actively damped with an electromagnetic damper. A closed-loop inclination system levels the stand while an active cooling system minimizes thermal effects. The thrust stand incorporates an in situ calibration rig. The thrust of a 3.4 kW Hall thruster is measured for thrust levels up to 230 mN. The uncertainty of the thrust measurements in this experiment is +/-0.6%, determined by examination of the hysteresis, drift of the zero offset and calibration slope variation.

Entities:  

Year:  2009        PMID: 19485530     DOI: 10.1063/1.3125626

Source DB:  PubMed          Journal:  Rev Sci Instrum        ISSN: 0034-6748            Impact factor:   1.523


  1 in total

1.  Recommended Practice for Thrust Measurement in Electric Propulsion Testing.

Authors:  James E Polk; Anthony Pancotti; Thomas Haag; Scott King; Mitchell Walker; Joseph Blakely; John Ziemer
Journal:  J Propuls Power       Date:  2017-04-24       Impact factor: 1.500

  1 in total

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