Integration of an Arcjet System on the Modular STB Lightsat Platform
The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory
A Modular Satellite Bus for the "Romolo & Remo" Dual Lightsat Magnetosphere Analysis Mission
Experimental Analysis of a Solid Propellant MPD Thruster with Different Anode Radii
Low cost access to Mars-Mars micromissions spacecraft
Advanced Propulsion System Options for Geostationary Satellites
Space technology three: mission overview and spacecraft concept description
Scale Effects On Solid Propellant MPD Thruster Performance