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Geometric Effects on Critical Heat Flux on Horizontal Microporous Coatings
Influence of Contact Angle and Tube Size on Capillary-Driven Flow Under Microgravity
Constrained Vapor Bubble Heat Pipe Experiment Aboard the International Space Station
High-Temperature Lm Cathode Ion Thrusters Quarterly Progress Report, 5 Feb. - 4 May 1968
Exploring in Aerospace Rocketry. 8 - Zero Gravity Effects
Development of an Infrared Imaging System for the Surface Tension Driven Convection Experiment
Multiphase Flow Research on the International Space Station
Gravity Dependent Two-Phase Research at the NASA Glenn Research Center
Technology for Subsystems of Space-Based Plant Growth Facilities
In-Orbit Demonstration of Two-Phase Heat Transport Technology: TPX/G557 Flight Results