Advanced propulsion system options for geostationary satellites
Advanced Propulsion System Options for Geostationary Satellites
Integration of an Arcjet System on the Modular STB Lightsat Platform
The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory
The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory
Integration of an Arcjet System on the Modular STB Lightsat Platform
Development and Testing of a New Thermal Protection Material for Reentry Vehicles
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
Space technology three: mission overview and spacecraft concept description
Scale Effects On Solid Propellant MPD Thruster Performance