Email this article To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
- Authors: Pelevin F.V.1, Ponomarev A.V.1
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Affiliations:
- Bauman Moscow State Technical University (National Research University)
- Issue: Vol 61, No 1 (2018)
- Pages: 71-77
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230409
- DOI: https://doi.org/10.3103/S1068799818010117
- ID: 230409
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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.
About the authors
F. V. Pelevin
Bauman Moscow State Technical University (National Research University)
Author for correspondence.
Email: pelfv@rambler.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
A. V. Ponomarev
Bauman Moscow State Technical University (National Research University)
Email: pelfv@rambler.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
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