Two‐phase flow characterization for fluid components and variable gravity conditions Available to Purchase

This paper describes a program initiated by the NASA Johnson Space Center to investigate vapor‐liquid flow regimes and pressure drops in pipe components and variable gravity conditions. This program supports the Space Station Freedom External Active Thermal Control System design and future space missions, including the Space Exploration Initiative activities. The objectives for this program include studying two‐phase flow behavior in fluid components (smooth pipes, bellows lines, quick‐disconnect fittings), expanding the two‐phase database for zero‐g conditions, developing a database for low‐g conditions (for example, Moon‐g, Mars‐g), and validating models for two‐phase flow analyses. Zero‐g and low‐g data will be gathered using a Freon‐12 flow loop during four test series on the KC‐135 aircraft beginning in August 1991.