NASA NTRS · 19720000407
Turbopump thermodynamic cooling
Abstract
System for cooling turbopumps used in cryogenic fluid storage facilities is described. Technique uses thermodynamic propellant vent to intercept pump heat at desired conditions. Cooling system uses hydrogen from outside source or residual hydrogen from cryogenic storage tank.
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Patten, T. C., Mckee, H. B.. 1972-07-01. Turbopump thermodynamic cooling. https://ntrs.nasa.gov/citations/19720000407
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