TY - GEN
T1 - Lithium purification system development for long-life lithium-fed lorentz force accelerators
AU - Stubbers, Robert A.
AU - Jurczyk, Brian E.
AU - Sander, Jonathan J.
AU - Brenner, Paul W.
AU - Wilson, John A.
AU - Coventry, Matthew D.
AU - Rovey, Joshua L.
AU - Alman, Darren A.
PY - 2007
Y1 - 2007
N2 - Lithium is an attractive metal propellant for advanced nuclear-electric propulsion missions because its low molecular weight results in high Isp and high conductivity for advanced MPD thrusters. The ALFA2 NASA program investigated a liquid lithium MPD thruster to support a > 5 year mission. Unfortunately, lithium is corrosive to most metals, leeches elements from alloys, destroys dielectric insulators, and is prone to contamination. Therefore, long-duration deep space missions using lithium will only be possible if these adverse effects can be mitigated or eliminated. For the ALFA 2 NASA mission, cathode erosion and work function poisoning due to impurities (notably oxygen) was observed and severely limits lifetime. Using a lithium purification and filtration system with highly porous gettering materials in series with cold trap filters is a possible way of reducing lithium contamination levels; thereby improving thruster lifetime. A proof-of-concept experiment was carried out to examine cold filtering and evaluate several candidate getter materials for purification. The long-term goal is to develop an active filtering and purification system for the ALFA2 thruster, or other lithium/liquid metal fed thrusters, to mitigate contamination effects for long-duration (>5 years) space missions. Starfire Industries successfully demonstrated: (1) reduction in impurity content by filtration, (2) regeneration of the filter assembly, (3) getter operation and regeneration, and (4) established a baseline for designing a prototype for a laboratory-scale thruster. These advances increase the regenerable filtration and gettering concept from TRL 1 to TRL 3. In addition, significant mass reduction is realized when compared to getter-only purification schemes that would likely perform poorer than the described system.
AB - Lithium is an attractive metal propellant for advanced nuclear-electric propulsion missions because its low molecular weight results in high Isp and high conductivity for advanced MPD thrusters. The ALFA2 NASA program investigated a liquid lithium MPD thruster to support a > 5 year mission. Unfortunately, lithium is corrosive to most metals, leeches elements from alloys, destroys dielectric insulators, and is prone to contamination. Therefore, long-duration deep space missions using lithium will only be possible if these adverse effects can be mitigated or eliminated. For the ALFA 2 NASA mission, cathode erosion and work function poisoning due to impurities (notably oxygen) was observed and severely limits lifetime. Using a lithium purification and filtration system with highly porous gettering materials in series with cold trap filters is a possible way of reducing lithium contamination levels; thereby improving thruster lifetime. A proof-of-concept experiment was carried out to examine cold filtering and evaluate several candidate getter materials for purification. The long-term goal is to develop an active filtering and purification system for the ALFA2 thruster, or other lithium/liquid metal fed thrusters, to mitigate contamination effects for long-duration (>5 years) space missions. Starfire Industries successfully demonstrated: (1) reduction in impurity content by filtration, (2) regeneration of the filter assembly, (3) getter operation and regeneration, and (4) established a baseline for designing a prototype for a laboratory-scale thruster. These advances increase the regenerable filtration and gettering concept from TRL 1 to TRL 3. In addition, significant mass reduction is realized when compared to getter-only purification schemes that would likely perform poorer than the described system.
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M3 - Conference contribution
AN - SCOPUS:36749049287
SN - 1563479036
SN - 9781563479038
T3 - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
SP - 2815
EP - 2821
BT - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
T2 - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Y2 - 8 July 2007 through 11 July 2007
ER -