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