Internal Langmuir Probe Mapping of a Hall Thruster With Xenon and Krypton Propellant

doi 10.2514/6.2006-4470
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Investigations of Probe Induced Perturbations in a Hall Thruster

2002English

Influence of Azimuthally Nonuniform Propellant Flow Rate on Thrust Vector and Discharge Current Oscillation in a Hall Thruster

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
2009English

Hall Thruster Erosion

2019English

Examination of a Hall Thruster Start Transient

2002English

Plasma Properties Downstream of a Low-Power Hall Thruster

Physics of Plasmas
Condensed Matter Physics
2005English

Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster

Journal of Propulsion and Power
SpacePlanetary ScienceFuel TechnologyMechanical EngineeringAerospace Engineering
1998English

Measurements of Wave Lengths in the Spectra of Krypton and Xenon

Scientific Papers of the Bureau of Standards
1919English

Determination of the Hall Thruster Operating Regimes

2002English

Bonding Xenon and Krypton on the Surface of Uranium Dioxide Single Crystal

Nukleonika
InstrumentationRiskWaste ManagementDisposalNuclear EnergyHigh Energy PhysicsEngineeringReliabilitySafetyNuclearQualityCondensed Matter Physics
2014English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy