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.
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Research Article|
May 06 2009
High-power, null-type, inverted pendulum thrust stand
Kunning G. Xu;
Kunning G. Xu
Department of Aerospace Engineering, High-Power Electric Propulsion Laboratory, Georgia Institute of Technology,
College of Engineering
, Atlanta, Georgia 30332, USA
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Mitchell L. R. Walker
Mitchell L. R. Walker
Department of Aerospace Engineering, High-Power Electric Propulsion Laboratory, Georgia Institute of Technology,
College of Engineering
, Atlanta, Georgia 30332, USA
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Rev. Sci. Instrum. 80, 055103 (2009)
Article history
Received:
January 21 2009
Accepted:
April 07 2009
Citation
Kunning G. Xu, Mitchell L. R. Walker; High-power, null-type, inverted pendulum thrust stand. Rev. Sci. Instrum. 1 May 2009; 80 (5): 055103. https://doi.org/10.1063/1.3125626
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