C~6~0 Application to Ion Thruster -Diagnostics of Electron Bombardment Plasma-
Evaluation of Electrodynamic Tether Propulsion to OTV
Experimental Study on Hollow Cathode Plasma Contactors
Feasibility Study of Pulsed Plasma Thruster for Micro- and Nano- Satellite
Interaction between Plasma Plume of Electric Propulsion and Spacecraft Communication
Investigation of Ion Beam Extraction Phenomena Using a Particle Simulation Code
Investigation of Scaling Law for Electrodynamic Tether Ground Experiments
Performance of Electrodynamic Tether De-Orbit System of Used H-II Upper Stage
Preliminary Experiments on Pulsed Plasma Thruster for Small Satellite
Preliminary Life Test of a Low-Power DC Arcjet Anode
R&D on Low Power Pulsed Plasma Thruster System for mu-Lab Sat II
R&D on Pulsed Plasma Thruster for mu-Lab Sat II - Development Status of EM -
Study of Small Helicon Plasma Source for Electric Propulsion Applications
Study on C~6~0 Application to Ion Thruster-Its Advantages and Present Status-