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High Performance Plasma Channel Insulators for High Power Hall Thrusters
Completed
TRL 3 (started at 1, targeting 3)
Description
NASA missions for planetary exploration require high power, long-life Hall thrusters. However, thruster power and lifetime are limited by the erosion of plasma channel walls. Current plasma channel insulator materials, such as BN or Borosil, have the required low secondary electron emission (SEE) but are susceptible to xenon plasma erosion. New plasma channel insulator materials with low SEE yield and high xenon plasma erosion resistance are needed to increase the efficiency and the lifetime of Hall thrusters. AlN has an exceptionally high plasma erosion resistance but suffers from a high SEE yield. AlN can be a "revolutionary" replacement for BN channel insulator since it provides high plasma erosion resistance with structural robustness and high thermal conductivity if it's SEE yield can be reduced. This SBIR Phase I program will develop a revolutionary AlN plasma channel insulator with lower SEE yield and higher erosion resistance than BN and BN-SiO2 for high power, long-life Hall thrusters. In Phase I we will (i) reduce the SEE yield of AlN by microstructural engineering, and (ii) fabricate fully functional plasma channel insulators for thruster testing at NASA-GRC to determine if the reduction of SEE yield of AlN channel insulator leads to better thruster performance than BN channels.
Benefits
High specific impulse, high power Hall thrusters will be key for planetary exploration and efficient cargo delivery to Mars. Project Prometheus would significantly benefit from the long-life, high power Hall thrusters afforded by the proposed channel insulators. Long-life, high power Hall thrusters would be useful in geosynchronous communications satellites to reduce propellant mass and as primary propulsion in deep space scientific missions.
The United States Air Force has many missions that would benefit from small, low-cost satellites. Commercial applications include communications and imaging satellites, companions to large satellites to provide surveillance and close-up inspection capabilities, such as to monitor and assure proper deployment of solar panels, antennae and other appendages.
Details
| Technology area | Propulsion Systems > Electric Space Propulsion > Electrostatic Propulsion |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Sienna Technologies, Inc., Woodinville, WA |
| Start date | 2013-05-23 |
| End date | 2013-11-23 |
Project contacts
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This is early/mid-stage (TRL 3) — 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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