Abstract This paper demonstrates that in transition from the one-dimensional longitudinal-channel motion of the coolant in the regenerative cooling system of the liquid propellant engine to the twodimensional (interchannel) channel motion (transpiration) through a porous mesh material (PMM), the hydraulic losses decrease. Experimental data on PMM hydraulic resistance coefficients and heat transfer in porous paths with the interchannel coolant transpiration (ICCT) is presented.
To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
Russian Aeronautics ; 61 , 1 ; 71-77
2018-01-01
7 pages
Article (Journal)
Electronic Resource
English
To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
Online Contents | 2018
|Transpiration And Regenerative Cooling Of Rocket Engine
NTRS | 1989
|SLUB | 1947
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