Electric Propulsion Characterization

SPL prides itself in being at the cutting edge of electric propulsion characterization techniques. Our MIT lab space has multiple high-vacuum test facilities outfitted with full suites of ion beam diagnostic instruments including time-of-flight mass spectrometers (TOF), retarding potential analyzers (RPA), Faraday probes, residual gas analyzers (RGA), and more. We also have a custom-built magnetically levitated thrust stand, allowing us to easily validate our ion beam measurements.

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Direct Thrust Measurement: MagLev Test Stand

Magnetically levitated thrust stand (MagLev) in SPL’s Astrovac facility.

Comparison of direct thrust measurements from the MagLev thrust stand to indirect thrust estimates inferred from time-of-flight.

Ion Beam Diagnostics

Diagnostic instruments in SPL’s Turbovac high-vacuum facility.

Clockwise from the top left: current-voltage (IV) curves, time-of-flight (TOF) curves, retarding potential analysis (RPA) measurements, angular beam distributions.

Advanced Characterization Techniques

Angular-resolved time-of-flight mass spectrometry.

Electrochemical decomposition of ionic liquid.

Relevant Publications