Matthew E. Moran

• Conceptual study of on orbit production of cryogenic propellants by water electrolysis
• Hydrogen no-vent fill testing in a 1.2 cubic foot (34 liter) tank
• Hydrogen no-vent fill testing in a 5 cubic foot (142) liter tank using spray nozzle and spray bar liquid injection
• Liquid Transfer Cryogenic Test Facility
• Micro-scale avionics thermal management
• Thermal control subsystem design for the avionics of a space station payload