Low cost access to Mars-Mars micromissions spacecraft
Space technology three: mission overview and spacecraft concept description
Experimental Analysis of a Solid Propellant MPD Thruster with Different Anode Radii
Scale Effects On Solid Propellant MPD Thruster Performance
Integration of an Arcjet System on the Modular STB Lightsat Platform
The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory
Integration of an Arcjet System on the Modular STB Lightsat Platform
The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory