Study on C~6~0 Application to Ion Thruster-Its Advantages and Present Status-
Study of Small Helicon Plasma Source for Electric Propulsion Applications
R&D on Pulsed Plasma Thruster for mu-Lab Sat II - Development Status of EM -
R&D on Low Power Pulsed Plasma Thruster System for mu-Lab Sat II
Preliminary Life Test of a Low-Power DC Arcjet Anode
Preliminary Experiments on Pulsed Plasma Thruster for Small Satellite
Performance of Electrodynamic Tether De-Orbit System of Used H-II Upper Stage