Thermal control subsystem design for the avionics of a space station payloadMatthew E. Moran · First published 1996Open the Tome
Hydrogen no-vent fill testing in a 5 cubic foot (142) liter tank using spray nozzle and spray bar liquid injectionMatthew E. Moran · First published 1992Open the Tome
Conceptual study of on orbit production of cryogenic propellants by water electrolysisMatthew E. Moran · First published 1991Open the Tome
Hydrogen no-vent fill testing in a 1.2 cubic foot (34 liter) tankMatthew E. Moran · First published 1991Open the Tome
