Dual-axis thrust stand for the direct characterization of electrospray performance

Abstract

A dual-axis torsional thrust stand was successfully demonstrated at the Air Force Research Laboratory, enabling direct simultaneous thrust and mass loss measurement for the Air Force Electrospray Thruster Series 2 passively fed electrospray thruster. The dual-axis system is effectively two nulled torsional thrust stands sharing a single dual-axis gimbal with a thrust and mass resolution of ±0.2 µN and ±0.04 mg, respectively. The development of this system was inspired by a need for direct efficiency characterization of electrosprays via in situ mass measurements, and performance was compared to thruster masses measured pre- and post-testing using an analytical balance. Mass consumption data captured via the dual-axis stand, which is calibrated to a traceable uncertainty of 1.6%, varied between −5% and 18% as compared to analytical balance measurements throughout a multi-month testing effort highlighting the limitations in pre/post-weighing as a method for capturing propellant consumption due to absorption of atmospheric moisture when thrusters are removed from vacuum. Thrust stand tests were limited to short term operation with a daily available testing window of ∼5 h due to thrust stand drift following the 24 h cyclic temperature variations of the testing facility. A thorough investigation into the root cause of ambient thermal drift suggests that the thermal response of commercial flex-pivot bearings is directly producing spurious torques on the order of 10 μN m/°C. Additionally, unresolved charging effects on thrust stand hardware currently limit thrust stand operation to tests operating with a positive thruster polarity. Further development and long duration test stability require both a targeted investigation into flex-pivot thermal response and minimization of facility effects.

Microgravity Decoupling in Torsion Pendulum for Enhanced Micro-Newton Thrust Measurement

“…Still, it is essential to implement an algorithm that can effectively correct any thermal drifts that may occur during thruster operation. Gilpin et al [14] believe that tilting causes the torsion pendulum to lose balance and changes its sensitivity, reducing its ability to respond to small torques; in addition, tilting introduces additional vibrations that affect the stability and accuracy of the torsional pendulum. Zhang et al [15] developed and validated a micro-Newton torsional thrust balance for an ionic liquid electrospray thruster.…”