J. Snyder

发表

Facility pressure effects on a Hall thruster with an external cathode: I. Numerical simulations

I. Mikellides, A. L. Ortega, V. Chaplin, 2020, Plasma Sources Science and Technology.

Facility pressure effects on a Hall thruster with an external cathode, II: theoretical model of the thrust and the significance of azimuthal asymmetries in the cathode plasma

I. Mikellides, A. L. Ortega, V. Chaplin, 2020, Plasma Sources Science and Technology.

Wear test of a magnetically shielded Hall thruster at 3000 seconds specific impulse IEPC-2013-033

I. Mikellides, J. Polk, R. Hofer, 2013 .

Electric Propulsion for the Psyche Mission

I. Mikellides, D. Goebel, A. L. Ortega, 2019 .

Mechanism Behind the Dependence of Thrust on Facility Backpressure and Implications on the Operation of the SPT-140 Onboard the Psyche Mission

I. Mikellides, A. L. Ortega, V. Chaplin, 2019 .

Review of carbon-based grid development activities for ion thrusters

John Steven Snyder, J. Snyder, 2003 .

Investigation of the feasibility of fullerene propellant for ion thrusters

J. Snyder, 1998 .

Results of a 1000-Hour Wear Test of 30-cm-Diameter Carbon-Carbon Ion Optics

J. Brophy, John R. Anderson, J. Snyder, 2005 .

Effects of Background Pressure on SPT-140 Hall Thruster Performance

Jason D. Frieman, T. Haag, J. Mackey, 2020 .

Peak Power Tracking and Multi-Thruster Control in Direct Drive Systems

J. Brophy, J. Snyder, 2013 .

FORWARD ERROR CORRECTION FOR SATELLITE TDMA IN THE INTELSAT V ERA

Takuro Muratani, John S. Snyder, J. Snyder, 1980 .

The Effects of Background Pressure on SPT-140 Hall Thruster Performance

Jason D. Frieman, T. Haag, J. Mackey, 2018, 2018 Joint Propulsion Conference.

Pre-Flight Assessment of Xenon Propellant Usage and Usage Uncertainty for the Psyche Mission

J. Snyder, Ian k. Johnson, Taylor Kerl, 2021, AIAA Propulsion and Energy 2021 Forum.

Simplified Ion Thruster Xenon Feed System For

D. Goebel, R. Hofer, T. Randolph, 2009 .

Neutralizer Hollow Cathode Simulations and Validation with Experiments

Dan M. Goebel, Ioannis G. Mikellides, John Steven Snyder, 2009 .

The discharge plasma in ion engine neutralizers: Numerical simulations and comparisons with laboratory data

I. Mikellides, I. Katz, D. Goebel, 2010 .

Performance Evaluation of the XIPS 25-cm Thruster for Application to NASA Discovery Missions

Dan M. Goebel, John Steven Snyder, Dan M. Goebel, 2006 .

Throttled Performance of the SPT-140 Hall Thruster

John Steven Snyder, Richard R. Hofer, R. Hofer, 2014 .

A high power ion thruster for deep space missions.

Anita Sengupta, D. Goebel, J. Polk, 2012, The Review of scientific instruments.

Performance Evaluation of the T6 Ion Engine

James E. Polk, Dan M. Goebel, John Steven Snyder, 2010 .

Solar Electric Propulsion for Discovery-Class Missions

Dan M. Goebel, John Steven Snyder, Richard R. Hofer, 2014 .

Solar Electric Propulsion Gravity-Assist Tours For Jupiter Missions

Nathan J. Strange, Damon Landau, John Steven Snyder, 2012 .

Electric Propulsion for the Psyche Mission: Development Activities and Status

I. Mikellides, D. Goebel, R. Hofer, 2020, AIAA Propulsion and Energy 2020 Forum.

Solar Electric Propulsion for Discovery Class Missions IEPC-2013-124

D. Goebel, R. Hofer, D. Oh, 2013 .

A 1-D Model of the Hall-Effect Thruster with an Exhaust Region

Ira Katz, J. Steven Snyder, I. Katz, 2001 .

Spacecraft Interaction Test Results of the High Performance Hall System SPT-140 (Postprint)

Lee S. Mason, Robert S. Jankovsky, Alec D. Gallimore, 2000 .

Evaluation of a 4.5 kW Commercial Hall Thruster System for NASA Science Missions

John Steven Snyder, Richard R. Hofer, David Y. Oh, 2006 .