Dependence of Plasma Velocity Exhausted From Quasi-Steady MPD Thrusters on Discharge Chamber Configurations.

Journal of the Japan Society for Aeronautical and Space Sciences
doi 10.2322/jjsass.48.129
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Plasma Acceleration Processes in a Quasi-Steady MPD Channel.

Journal of the Japan Society for Aeronautical and Space Sciences
1998English

Critical Technology Demonstration of Plasma Focus Type MPD Thrusters

1992English

Effects of Ignition on Discharge Symmetry in Gas-Fed Pulsed Plasma Thrusters

1998English

Effects of Flow Measurement Resolution on Quasi-Steady Body Force Estimation in Dielectric-Barrier-Discharge Plasma Actuator

AIP Advances
NanotechnologyAstronomyPhysicsNanoscience
2016English

Stable Plasma Configurations in a Cylindrical Magnetron Discharge

Applied Physics Letters
AstronomyPhysics
2004English

Modular Coils and Plasma Configurations for Quasi-Axisymmetric Stellarators

2010English

Performance of an Applied Field MPD Thruster With a Pre-Ionization Chamber

2002English

Dependence of the Transition From Townsend to Glow Discharge on Secondary Emission

Physical Review E
2004English

Ejected Plasma Parameters From Coaxial Discharge

The International Conference on Electrical Engineering
1999English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy