Engineering topics
Katz, I.
Publications and source records attributed to Katz, I..
Detection of Organic Constituents Including Chloromethylpropene in the Analyses of the ROCKNEST Drift by Sample Analysis at Mars (SAM)
key challenge in assessing the habitability of martian environments is the detection of organic matter - a requirement of all life as we know it. The Curiosity rover, which landed on August 6, 2012 in Gale Crater of Mars, includes the Sample Analysis at Mars (SAM) instrument suite capable of in situ analysis of gaseous organic components thermally evolved from sediment samples collected, sieved, and delivered by the MSL rover. On Sol 94, SAM received its first solid sample: scooped sediment from Rocknest that was sieved to <150 m particle size. Multiple 10-40 mg portions of the scoop #5 sample were delivered to SAM for analyses. Prior to their introduction, a blank (empty cup) analysis was performed. This blank served 1) to clean the analytical instrument of SAMinternal materials that accumulated in the gas processing system since integration into the rover, and 2) to characterize the background signatures of SAM. Both the blank and the Rocknest samples showed the presence of hydrocarbon components.
Estimation of Hall thruster erosion using HPHall
The erosion of the acceleration channel walls of magnetic layer Hall thrusters is one of the mechanism limiting the lifetime of this technology.
Model of the plasma potential distribution near the discharge cathode in an ion thruster
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Numerical simulation of two-grid ion optics using a 3D code
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A high power ion thruster plume model
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The status of ion propulsion development and implementation at JPL in 2003
The successful demonstration of ion propulsion on NASA's Deep Space 1 mission has stimulated substantial interest in the application of this technology to future solar system exploration missions.
Technologies to improve ion propulsion system performance, life and efficiency for NEP applications
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Technologies to improve ion propulsion system performance, life and efficiency for NEP
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Model of hollow cathode operation and life limiting mechanisms
In this paper we apply results from the extensive traveling wave tube vacuum barium impregnated cathode literature to the hollow cathodes used in ion thrusters. We show that the observed space station cathode life is in general agreement with published barium evaporation rates.
Technologies to improve ion propulsion system performance, life and efficiency for NEP
In this paper we present ion thruster design concepts created using the new computer codes that model performance limiting and erosion mechanisms. Presently, the codes model extraction grid ion optics and both discharge and neutralizer hollow cathodes.
Plasma generation near an ion engine discharge chamber hollow cathode
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Electric propulsion at the Jet Propulsion Laboratory
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Numerical simulations of ion thruster accelerator grid erosion
The highly successful demonstration of ion propulsion on Deep Space 1 has stimulated the study of more demanding applications of ion propulsion. These future applications require ion thrusters capable of providing significantly greater specific impulses and total impulses than the current state-of-the-art Higher specific impulses aggravate the known wear out mechanisms of the ion accelerator system.
A model of hollow cathode plasma chemistry
We have developed a new model of hollow cathode plasma chemistry based on the observation that xenon ion mobility is diffusion limited due to resonant charge exchange reactions. The model shows that vapor phase barium atoms are ionized almost immediately and electric fields accelerate the ions upstream from the emission zone. We have also applied the model to the orifice region, where the resultant ion generation profile correlates with previously reported orifice erosion.
A model of hollow cathode plasma chemistry
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High efficiency, high power ion thrusters for operation at specific impulses greater than 7000 s
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Long life hollow cathodes for high power NEP missions
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