Session
Pre-Conference Poster Session II
Location
Utah State University, Logan, UT
Abstract
Propulsion has been identified as a critical capability for future SmallSat and CubeSat missions. Due to strict volume constraints imposed by these small platforms, efficient means of propulsion is key to enabling sophisticated missions with large payload mass fraction and ΔV.
Pure Ionic Electrospray Thruster Control Electronics Architecture and Performance
Utah State University, Logan, UT
Propulsion has been identified as a critical capability for future SmallSat and CubeSat missions. Due to strict volume constraints imposed by these small platforms, efficient means of propulsion is key to enabling sophisticated missions with large payload mass fraction and ΔV.