David J. Chato
Analysis of the nonvented fill of a 4.96-cubic-meter lightweight liquid hydrogen tank
Cryogenic transfer options for exploration missions
Ground testing for the no-vent fill of cryogenic tanks
Ground testing on the nonvented fill method of orbital propellant transfer
Initial experimentation on the nonvented fill of a 0.14 m³ (5 ft³) dewar with nitrogen and hydrogen
Review and test of chilldown methods for space-based cryogenic tanks
Small experiments for maturation of orbital cryogenic transfer technologies
Status and design concepts for the hydrogen on-orbit storage and supply experiment
Thermodynamic modeling of the no-vent fill methodology for transferring cryogens in low gravity
Vented tank resupply experiment--flight test results