Enviar artigo por via de e-mail To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
- Autores: Pelevin F.V.1, Ponomarev A.V.1
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Afiliações:
- Bauman Moscow State Technical University (National Research University)
- Edição: Volume 61, Nº 1 (2018)
- Páginas: 71-77
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230409
- DOI: https://doi.org/10.3103/S1068799818010117
- ID: 230409
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Resumo
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.
Sobre autores
F. Pelevin
Bauman Moscow State Technical University (National Research University)
Autor responsável pela correspondência
Email: pelfv@rambler.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005
A. Ponomarev
Bauman Moscow State Technical University (National Research University)
Email: pelfv@rambler.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005
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