Abstract
The combustion of kerosene with the polymer additive polyisobutylene (PIB) was experimentally investigated. The aim of the study was to measure the effect of PIB kerosene on the effciency of combustion chamber cooling and the combustion effciency of the liquid propellant for a rocket engine operating on kerosene and gaseous oxygen (GOX). The study was conducted on an experimental rocket engine using kerosene wall film cooling in the combustion chamber. Fire tests showed that the addition of polyisobutylene to kerosene had no significant effect on the combustion effciency. However, analysis of the wall temperature measurement results showed that the use of PIB kerosene is more effective for film cooling than pure kerosene, which can increase the effciency of combustion chamber cooling and subsequently increase its reliability and reusability. Thus, the findings of this study are expected to be of use in further investigations of wall film cooling effciency.
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CITATION STYLE
Borovik, I., Strokach, E., Kozlov, A., Gaponov, V., Chvanov, V., Levochkin, P., & Yoon, Y. (2019). Influence of polyisobutylene Kerosene additive on combustion effciency in a liquid propellant rocket engine. Aerospace, 6(12). https://doi.org/10.3390/aerospace6120129
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