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Current Issue

  • 2011,Vol 32,No. 6

    15 June 2011

Numerical simulation of perveance impingement current for ion thruster

2011, 32 (6): 751-755   

A theoretical study on the emitter apex and the mechanism of field emission electric propulsion thruster

2011, 32 (6): 756-761   

Method of improving beam current profile for ion thruster

2011, 32 (6): 762-765   

Probabilistic evaluation of ion thruster accelerator grid life

2011, 32 (6): 766-769   

Design of a Hall thruster with self-excited mode

2011, 32 (6): 770-775   

Numerical analysis on macro-characteristics of pulsed plasma thruster

2011, 32 (6): 776-780   

Design and experimental investigation of a single-coil SPT with low power

2011, 32 (6): 781-787   

Ablation modeling and simulation for pulsed plasma thruster

2011, 32 (6): 788-793   

Study on ionization characteristics of low power Hall thruster with variable cross-section channel

2011, 32 (6): 794-798   

Characteristics of magnetized sheath in Hall thruster

2011, 32 (6): 799-805   

Influences of discharge channel width on ionization characteristics in Hall thrusters

2011, 32 (6): 806-812   

Effects of non-Maxwellian electron distribution function on plasma-wall interaction in Hall thrusters

2011, 32 (6): 813-817   

Wavelet solution of one-dimensional hydrodynamic mode of a Hall thruster

2011, 32 (6): 818-822   

Effects of a new buffer magnetic circuit on preionization and discharge in a P70 Hall thruster

2011, 32 (6): 823-827   

Comparison for the Hall thruster using Xe and Kr propellent

2011, 32 (6): 828-834   

Experimental investigation on pulsed high-voltage cylindrical anode layer Hall plasma accelerator

2011, 32 (6): 835-838   

Numerical simulation of the stationary plasma thruster plume and its effects on the microwave attenuation and phase shifts

2011, 32 (6): 839-844   

Development of the 1kW class hydrazine arcjet

2011, 32 (6): 845-851   

Effects of nozzle temperature on performance of low power arcjet thrusters

2011, 32 (6): 852-856   

Progress on the research of helicon plasma thruster

2011, 32 (6): 857-863   

Effects of the nozzle configuration on the impulse coupling coefficient for multi-pulsed laser propulsion

2011, 32 (6): 864-868   

Experiment and numerical simulation for propagating and mixing process of the plasma jet in liquid medium

2011, 32 (6): 869-877   

Double-electrostatic probe measurements of electron temperature and electron number density in an arcjet thruster plume

2011, 32 (6): 878-881   

LabVIEW-based multi-probe plasma diagnosis system

2011, 32 (6): 882-888   

Single langmuir probe measurement in the exit plasma of an arcjet thruster

2011, 32 (6): 889-894   

Directional probe measurement of plume divergence angle in Hall thrusters

2011, 32 (6): 895-899