11th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics TEMPERATURE MEASUREMENTS IN A MULTIPHASE FLUID HAMMER López Peña, F.* and Lema M. *Author for correspondence Department of Marine and Oceanic Engineering, University of A Coruña, Rúa da Maestranza, 9 15001 A Coruña, Spain E-mail:
[email protected] Rambaud P. and Buchlin J-M Steelant J. von Karman Institute for Fluid Dynamics Propulsion Design and Aerothermodynamics Section Chaussée de Waterloo 72, B-1640 Rhode-St-Genèse European Space Agency Belgium Keplerlaan 1, P.O. Box 299, 2200 AG Noordwijk, The Netherlands ABSTRACT subject of interest on liquid propulsion systems, mainly related Any satellite propulsion system is inactive at launching, to the analysis of the flow transients. One of the first studies having the liquid propellant confined into tanks and the found on this subject was presented by Yaggy [1], where he propellant lines vacuum pumped or filled with a non- modeled two pipe segments separated by an isolation valve and condensable gas (NCG) at low pressure. Once in orbit, the using real propellants. The author performs a numerical propulsion system performs the so-called priming maneuver analysis of this configuration, varying the two pipes length, and that consists in filling these lines with the pressurized liquid the initial pressure conditions downstream, concluding that propellant (hydrazine), by opening a fast isolation valve. The friction played an important role, where the greater unsteady opening of this valve subsequently induces a fluid hammer, friction factor, compared to the steady value, substantially together with various multiphase phenomena, such as cavitation reduces the pressure surges.