Working Group 5: Measurements Technology and Active Experiments
What Processes Influence Plasmaspheric Refilling?
Vehicle Charging of the Shuttle Orbiter During Electron Beam Emission
Using Additive Manufacturing to Print a CubeSat Propulsion System
Using Additive Manufacturing to Print a CubeSat Propulsion System
Use of Electrostatic Propulsion at Lower Exhaust Velocities
Use of Dried Plasma in Prehospital Battlefield Resuscitation 2011-04
Unique Variable Polarity Plasma Arc Welding for Space Shuttle
Unified Approach to Computer Analysis and Modeling of Spacecraft Environmental Interactions
TROPIX: A Solar Electric Propulsion Flight Experiment
Transport Properties of Partially Ionized Nitrogen. I - the Collision Integrals
Transport Properties of Partially Ionized Nitrogen. II - Method and Results