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Re-generable Field Emission Cathodes

Completed TRL 5 (started at 4, targeting 5)

Description

A significant challenge in scaling micro-propulsion devices up to 100s of Watts as well as scaling macro devices down to sub-kiloWatt level is the lack of a compatible neutralizer technology in the meso scale. Sub-kiloWatt EP systems require cathode technology that can produce sufficient current while consuming little or no gas or power. The most promising technology for meso-scale neutralizers is field emission. In field emission, electrons are extracted directly from a cold bulk solid material by an intense applied electric field at the solid-vacuum interface with no gas flow and no heating required. While many methods have been proposed to incorporate field-emission neutralizers in EP systems, the inherent fragility of the technology – specifically the reliance on solid structures with nanometer-radius tips – ensures that device failure due to tip degradation will be a near certainty for any application depending on field emission cathodes. The goal of research proposed here is to develop arrays of field-emission neutralizers for use in sub-1-kW EP that eliminate tip degradation not through attempts to minimize tip wear, but instead by incorporating self-assembling nanostructures that can repeatedly re-generate damaged emitter tips in space and fully restore the functionality of a damaged or degraded device.

Benefits

Proposed technology could be used for any function requiring electron emission in space. Potential applications include spacecraft neutralizers, space weather diagnostic sensors, electrodynamic tethers, and sub-1-kW electric propulsion systems for space science missions.

Electron field emitters are use in numerous applications including electron microscopes, flat panel displays, and microwave generators.

Details

Technology areaPropulsion Systems > Electric Space Propulsion > Electrostatic Propulsion
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationAerophysics, Inc., Allouez, MI
Start date2013-05-23
End date2013-11-23

Project contacts

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How to get involved

This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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