1-D Thermal Simulation and Experimental Validation of Li-Ion Battery Pack Liquid Cooling System
3.2 KWH Battery Pack Using 18 Army Standard Lithium ion Rechargeable Batteries
3D Formation Flight Using Differential Carrier-Phase GPS Sensors
3D Image-based Navigation in Collaborative Navigation Environment
6-ft High-Power Electric Propulsion Test Port, EPL Tank 5 Installed
8-cm Ion Thruster Characterization
16.522 Space Propulsion, Spring 2004.
Space Propulsion
50 to 100 Ah lithium-ion cells for aircraft and spacecraft applications
1000 Hours of Testing Completed on 10-kW Hall Thruster
2000 Dollar Electric Powertrain Option-1 Program. Final technical report
A 2-D comparison of ionospheric convection derived from SuperDARN and DMSP measurements
A 2-D model of a hollow cathode insert plasma
A 100 Hour Wear Test of the NASA NSTAR Ion Thruster
A balancing and monitoring system for battery cell stacks in electrical vehicles
A Battery Certification Testbed for Small Satellite Missions