Abstract
An efficient long-term storage of cryogenic propellants is a challenge for future space exploration missions. The vapour bubbles formed as a result of boil-off in the tank walls can generate foam structures, which could be hazardous in different operations in orbit. A recently proposed approach to control the dynamics of bubbles is based on the generation of an acoustic field by means of a piezoelectric transducer. This technology needs to be validated at cryogenic temperatures in order to be applicable in space. In this perspective, different piezoelectric elements and matching layer materials have been tested at cryogenic temperatures to assess their performance at such environmental conditions. We consider the use of soft PZT piezoceramics coupled with an epoxy resin as the matching layer. Experimental data reveal that epoxy resin-based acoustic matching layers exhibit a linear increase in the transmittance of the acoustic amplitude at cryogenic conditions. The peak-to-peak amplitude increases as temperature decreases up to a factor of 1.6. This result opens the possibility of generating and transmitting acoustic waves at cryogenic temperatures, which could be used in the recently proposed technology to control the dynamics of vapour bubbles in cryogenic fuel tanks.
Similar content being viewed by others
References
Chato, D.J.: Low gravity issues of cryogenic fluid management technologies enabling exploration. National Academies (2009)
Crum, L.A.: Bjerknes forces on bubbles in a stationary sound field. J. Acoust. Soc. Am. 57, 1363 (1975)
Dodge, F.T.: The New Dynamic Behavior of Liquids in Moving Containers. Southwest Research Institute, San Antonio (2000)
Doherty, M.P., Gaby, J.D., Salerno, L.J., Sutherlin, S.G.: Cryogenic fluid management technology for moon and mars missions, Technical Report TM-2010-216070 NASA (2010)
Donabedian, M.: Editor: Spacecraft Thermal Control Handbook, vol. 2, Cryogenics. The Aerospace Press, El Segundo (2003)
Glover, D.: NASA cryogenic fluid management space experiment efforts 1960-1990, Technical Report TM-103752 NASA (1991)
Hotate, M., Yoshidome, D., Kojima, T., Hoshina, T., Takeda, H., Tsurumi, T: Design and fabrication of acoustic matching layer for lead-free ultrasonic flowmeter. J. Ceramic Soc. Japan 123(5), 317–321 (2015)
Lacovic, R.F., Yeh, F.C., Szabo, S.V., Brun, R.J., Stofan, A.J., Berns, J.A.: Management of cryogenic propellants in a full-scale orbiting space vehicle, Technical Report TN D-4571 NASA (1968)
Leighton, T.G.: The Acoustic Bubble. Academic Press, New York (1974)
López-martínez, G., González-cinca, R.: Acoustic control of boiling dynamics under microgravity (in preparation) (2020)
Motil, S.M., Meyer, M.L., Tucker, S.P.: Cryogenic fluid management technologies for advanced green propulsion systems, Technical Report TM-2007-214810 NASA (2007)
Muratov, C.B., Osipov, V.V., Smelyanskiy, V.N.: Issues of long-term cryogenic propellant storage in microgravity, Technical Report TM-2011-215988 NASA (2011)
Quintana-Buil, G., Garcia-Sabaté, A., Batlle, S., López, G., Sierra, V., Casas, O., González-cinca, R.: A sounding rocket experiment to control boiling by means of acoustic waves. Microgravity Sci. Technol. 29(5), 731–736 (2018)
Sutton, G.P., Biblarz, O.: Rocket Propulsion Elements. Wiley, Hoboken (2001)
Acknowledgements
This research was supported by the Agencia Estatal de Investigación (Spanish Government) project ESP2015-72277-EXP.
Author information
Authors and Affiliations
Corresponding author
Ethics declarations
Conflict of interests
The authors declare that they have no conflict of interest.
Additional information
Publisher’s Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
This article belongs to the Topical Collection: The Effect of Gravity on Physical and Biological Phenomena
Guest Editor: Valentina Shevtsova
Rights and permissions
About this article
Cite this article
Suñol, F., Ochoa, D.A., Granados, M. et al. Performance Assessment of Ultrasonic Waves for Bubble Control in Cryogenic Fuel Tanks. Microgravity Sci. Technol. 32, 609–613 (2020). https://doi.org/10.1007/s12217-020-09795-y
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12217-020-09795-y