Capillary Channel Flow (CCF) - 12.03.13
Science Objectives for Everyone
Capillary flow is the natural wicking of fluid between narrow channels in the opposite direction of gravity. Tree roots are one example of a capillary system, drawing water up from the soil. By increasing understanding of capillary flow in the absence of gravity, the Capillary Channel Flow (CCF) experiment helps scientists find new ways to move liquids in space. Capillary systems do not require pumps or moving parts, which reduces their cost, weight and complexity.
Science Results for Everyone
National Aeronautics and Space Administration (NASA)Sponsoring Organization
Human Exploration and Operations Mission Directorate (HEOMD)Research Benefits
Information PendingISS Expedition Duration:
September 2010 - March 2014Expeditions Assigned
25/26,27/28,29/30,33/34,35/36,37/38Previous ISS Missions
ISS Expedition 25/26 was the first operation of CCF in microgravity.
- Currently, spacecraft fuel tanks rely on an additional reservoir to prevent the ingestion of gas into the engines during firing. Research is required to update current models, which do not adequately predict the maximum flow rate achievable through the capillary vanes.
- CCF tests the theoretical predictions for the free surface shapes and the critical flow velocities for open capillary channel (vane) flows in microgravity. CCF is designed to validate the assumptions used to develop the governing equations. The experiments provide the verifications for the flow rate limits and corresponding critical flow velocities.
Capillary Channel Flow (CCF) is a versatile experiment for studying a critical variety of inertial-capillary dominated flows key to spacecraft systems that cannot be studied on the ground. The results of CCF will help innovate existing and inspire new applications in the portion of the aerospace community that is challenged by the containment, storage, and handling of large liquid inventories (fuels, cryogens, and water) aboard spacecraft. The results will be immediately useful for the design, testing, and instrumentation for verification and validation of liquid management systems of current orbiting, design stage, and advanced spacecraft envisioned for future lunar and Mars missions. The results will also be used to improve life support system design, phase separation, and enhance current system reliability.
Since hydrostatic pressure is absent in microgravity, technologies for liquid management in space use capillary forces to position and transport liquids. On Earth, the effect of capillary forces is limited to a few millimeters. In space, these forces still affect free surfaces that extend over meters. For the application of open channels in propellant tanks of spacecraft, design knowledge of the limitations of open capillary channel flow is a requirement.
Current spacecraft fuel tanks rely on an additional reservoir to prevent gases from entering the engines during firing. Capillary systems larger than a few millimeters in length are impossible to study on the ground, but the weightlessness on the International Space Station makes research on a variety of capillary channel sizes possible. The results are useful for the design and testing of liquid management systems in current use and for future missions.
Rocket fuel tank designs and construction models from space research help to advance new technology and manufacturing capabilities on Earth.
Forced liquid flows through open capillary channels with free liquid surfaces will be investigated in the Microgravity Science Glovebox (MSG) onboard ISS. In open capillary channels, if a certain critical flow rate is exceeded, the flow becomes unsteady, the surfaces collapse, and gas ingestion occurs at the outlet. From a fluid mechanical point of view, a characteristic critical velocity must exist at which the steady subcritical flow turns into an unsteady supercritical flow, which involves the collapse of the free surfaces. To find this velocity and the location of collapse of the free surface, the surface profile must be measured with great accuracy. Furthermore, the local flow velocity must be known at dedicated points of the channel.Operational Protocols
The crew involvement is limited to installation of the CCF hardware in the MSG work volume and exchange of experiment units between sessions.
Canfield P, Bronowicki PM, Chen Y, Kiewidt L, Grah A, Klatte J, Jenson RM, Blackmore W, Weislogel MM, Dreyer ME. The capillary channel flow experiments on the International Space Station: experiment set-up and first results. Experiments in Fluids. 2013 May 8; 54(5): 1519.
Ground Based Results Publications
CCF experimental unit and electrical subsystem, image courtesy of Glenn Research Center.
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