Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber

Nae, Catalin; Andrei, Irina-Carmen; Stroe, Gabriela-Liliana; Berbente, Sorin

Catalin Nae, Irina-Carmen Andrei, Gabriela-Liliana Stroe, Sorin Berbente

Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber

Abstract:

The chemical properties of the fuels are crucial for obtaining the numerical accuracy during the design and performance analysis in case of liquid fuel propelled rocket engines, as well as the trajectory optimization. In this paper, the research was primarly focused on optimizing the numerical accuracy for non-linear two-dimensional approximation the Fuel Combustion Charts; secondarily, the investigation was carried on the design of the bell-nozzle of a liquid propelled rocket engine, taking into account the variation of the coefficients which are significant for expressing the fuels chemical properties. From the Fuel Combustion Charts, the authors selected a the LOX - Kerosene combination for propelling the rocket engine, due to the most convenient matching with the technology and material specifications, safety and environmental friendly requirements; from the LOX-Kerosene Charts, the authors have originally developed a method to obtain the expression of a non-linear approximation function of two variables. The design of the bell shaped nozzle and combustion chamber for a liquid propelled rocket engine was included, in purpose to illustrate the link between the LPRE design and the fuels types and chemical properties.

Keywords:
fuel combustion charts; liquid propelled rocket engines; combustion chambers

Issue: 2020, Volume 71, Issue 1

Pages: 436-444

Publication date: 2020/2/7

https://doi.org/10.37358/RC.20.1.7872

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This article is published under the Creative Commons Attribution 4.0 International License

Citation Styles

Cite this article as:
NAE, C., ANDREI, I., STROE, G., BERBENTE, S., Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber, Rev. Chim., 71(1), 2020, 436-444.

Vancouver
Nae C, Andrei I, Stroe G, Berbente S. Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber. Rev. Chim.[internet]. 2020 Jan;71(1):436-444. Available from: https://doi.org/10.37358/RC.20.1.7872

APA 6th edition
Nae, C., Andrei, I., Stroe, G. & Berbente, S. (2020). Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber. Revista de Chimie, 71(1), 436-444. https://doi.org/10.37358/RC.20.1.7872

Harvard
Nae, C., Andrei, I., Stroe, G., Berbente, S. (2020). 'Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber', Revista de Chimie, 71(1), pp. 436-444. https://doi.org/10.37358/RC.20.1.7872

IEEE
C. Nae, I. Andrei, G. Stroe, S. Berbente, "Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber". Revista de Chimie, vol. 71, no. 1, pp. 436-444, 2020. [online]. https://doi.org/10.37358/RC.20.1.7872

Text
Catalin Nae, Irina-Carmen Andrei, Gabriela-Liliana Stroe, Sorin Berbente,
Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber,
Revista de Chimie,
Volume 71, Issue 1,
2020,
Pages 436-444,
ISSN 2668-8212,
https://doi.org/10.37358/RC.20.1.7872.
(https://revistadechimie.ro/Articles.asp?ID=7872)
Keywords: fuel combustion charts; liquid propelled rocket engines; combustion chambers

RIS
TY - JOUR
T1 - Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber
A1 - Nae, Catalin
A2 - Andrei, Irina-Carmen
A3 - Stroe, Gabriela-Liliana
A4 - Berbente, Sorin
JF - Revista de Chimie
JO - Rev. Chim.
PB - Revista de Chimie SRL
SN - 2668-8212
Y1 - 2020
VL - 71
IS - 1
SP - 436
EP - 444
UR - https://doi.org/10.37358/RC.20.1.7872
KW - fuel combustion charts
KW - liquid propelled rocket engines
KW - combustion chambers
ER -

BibTex
@article{RevCh2020P436,
author = {Nae Catalin and Andrei Irina-Carmen and Stroe Gabriela-Liliana and Berbente Sorin},
title = {Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine’s Bell Exhaust Nozzle and Combustion Chamber},
journal = {Revista de Chimie},
volume = {71},
number = {1},
pages = {436-444},
year = {2020},
issn = {2668-8212},
doi = {https://doi.org/10.37358/RC.20.1.7872},
url = {https://revistadechimie.ro/Articles.asp?ID=7872}
}

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