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Development of an Apparatus for Determining Surface Tension in Drops: Post-Flight Analysis of STS-108
Universidad Nacional del Comahue – Facultad de Ingenierk, Bs.As. 1400 – (8300) Neuquén Argentina. E-mail: lassig@uncoma.edu.ar
Fluid Dynamics & Materials Processing 2009, 5(1), 61-80. https://doi.org/10.3970/fdmp.2009.005.061
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This paper presents a description of the design and ensuing development of an automated liquid droplet generator and related utilization aboard the space shuttle, a) as a fluid positioning system for materials processing (attached droplet method), and b) as a means to measure surface oscillation of droplets under microgravity for determining their surface tension.Keywords
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APA Style
Lassig, , J., , Montes, , G., , Quiroga, et al. (2009). Development of an apparatus for determining surface tension in drops: post-flight analysis of STS-108. Fluid Dynamics & Materials Processing, 5(1), 61-80. https://doi.org/10.3970/fdmp.2009.005.061
Vancouver Style
Lassig , J. , Montes , G. , Quiroga , J. . Development of an apparatus for determining surface tension in drops: post-flight analysis of STS-108. Fluid Dyn Mater Proc. 2009;5(1):61-80 https://doi.org/10.3970/fdmp.2009.005.061
IEEE Style
Lassig, J., Montes, G., Quiroga, and J. "Development of an Apparatus for Determining Surface Tension in Drops: Post-Flight Analysis of STS-108," Fluid Dyn. Mater. Proc., vol. 5, no. 1, pp. 61-80. 2009. https://doi.org/10.3970/fdmp.2009.005.061
This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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