To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber


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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.

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F. Pelevin

Bauman Moscow State Technical University (National Research University)

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Email: pelfv@rambler.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005

A. Ponomarev

Bauman Moscow State Technical University (National Research University)

Email: pelfv@rambler.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005

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