Abstract
Today’s high-performance missiles and aircraft require propellant supply systems which carefully balance the following:
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1.
High speed and light weight of the pumps
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2.
Low tank pressurization for low tank weight
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3.
Steady and reliable propellant feed, free from cavitation surging
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References
R. C. Fisher, “Communications on Centrifugal Pumps for Oil Fields and Refineries,” Proc. ASME, Vol. 152 (1945).
R.B. Jacobs et al., “Research and Development Pumping of Cryogenic Fluids,” CBL-NBS Tech. Mem. 36 (Feb. 24. 1956).
H.A. Stahl and A. J. Stepanoff, “Thermodynamic Aspects of Cavitation in Centrifugal Pumps,” ASME Paper No. 55-A-136 (September, 1955).
A. Hollander, “Thermodynamic Aspects of Cavitation in Centrifugal Pumps.” private communication.
Pesco Products Division, Borg-Warner Corporation, selected published and unpublished data on pumping of liquid hydrogen; J. P. DiStefano and J. O. Panosian, “Cavitation Characteristics of Tank Mounted Centrifugal Type Cryogenic Pumps,” ASME Paper No. 61-AV-43 (1961);
G.H. Caine and S. Prelowski, “Results of a Study of Best Pumping System for a Liquid Parahydrogen Aircraft Fuel System,” WADC TR 58–679, ASTIA AD 304261 (1958).
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© 1962 Springer Science+Business Media New York
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DiStefano, J.F., Caine, G.J. (1962). Cavitation Characteristics of Tank-Mounted Cryogenic Pumps and Their Predicted Performance under Reduced Gravity. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 7. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0531-7_34
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DOI: https://doi.org/10.1007/978-1-4757-0531-7_34
Publisher Name: Springer, Boston, MA
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