Parametric investigation of orifice aspect-ratio on low current hollow cathode power consumption

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76725/1/AIAA-1998-3345-942.pd

A Hall probe diagnostic for low density plasma accelerators

A Hall probe diagnostic was developed for use with plasma thrusters. The Hall generators were mounted at the end of a stainless steel tube heat exchanger. Ceramic cement and a Pyrex tube were used as radiation and particle flux shields, respectively. A thermocouple was used to monitor the temperature of the Hall generator. The low voltage output from the probe was amplified within one meter of the transducer to minimize the effect of noise pick up. A National Institute of Standards and Technology traceable Gaussmeter provided an absolute reference for calibration, and relative calibrations were performed both in a strong electric field and in situ during thruster operation to approximate the conditions in the discharge. The overall accuracy of the diagnostic was ±6 G.±6G. The probes were tested with a Hall-effect thruster, and provided sufficiently accurate data to estimate the magnitude of the closed-drift electron current. © 1998 American Institute of Physics.Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/69868/2/RSINAK-69-6-2546-1.pd

The Status of Laser Diagnostics Supporting Ion Thruster Development at NASA GRC

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76321/1/AIAA-2002-3960-677.pd

Sensitivity of hollow cathode performance to design and operating parameters

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76435/1/AIAA-1999-2576-299.pd

Very near-field plume investigation of the D55

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76343/1/AIAA-1997-3062-753.pd

Low-current hollow cathode evaluation

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76856/1/AIAA-1999-2575-648.pd

IMECE2002-39444 ION ENGINE AND HALL THRUSTER DEVELOPMENT AT THE NASA GLENN RESEARCH CENTER

ABSTRACT NASA's Glenn Research Center has been selected to lead development of NASA's Evolutionary Xenon Thruster (NEXT) system. The central feature of the NEXT system is an electric propulsion thruster (EPT) that inherits the knowledge gained through the NSTAR thruster that successfully propelled Deep Space 1 to asteroid Braille and comet Borrelly, while significantly increasing the thruster power level and making improvements in performance parameters associated with NSTAR. The EPT concept under development has a 40 cm beam diameter, twice the effective area of the Deep-Space 1 thruster, while maintaining a relatively-small volume. It incorporates mechanical features and operating conditions to maximize the design heritage established by the flight NSTAR 30 cm engine, while incorporating new technology where warranted to extend the power and throughput capability. The NASA Hall thruster program currently supports a number of tasks related to high power thruster development for a number of customers including the Energetics Program (formerly called the Space-based Program), the Space Solar Power Program, and the In-space Propulsion Program. In program year 2002, two tasks were central to the NASA Hall thruster program: 1.) the development of a laboratory Hall thruster capable of providing high thrust at high power; 2.) investigations into operation of Hall thrusters at high specific impulse. In addition to these two primary thruster development activities, there are a number of other on-going activities supported by the NASA Hall thruster program. These additional activities are related to issues such as thruster lifetime and spacecraft integration. INTRODUCTION The success of the NASA Solar Electric Propulsion Technology Applications Readiness (NSTAR) program io

The D-100 performance and plume characterization on krypton

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76487/1/AIAA-1996-2969-208.pd

Laser induced fluorescence characterization of ions emitted from hollow cathodes

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76900/1/AIAA-1999-2862-539.pd

Near-field investigation of ions emitted from a hollow cathode assembly operating at low-power

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76514/1/AIAA-1998-3658-652.pd