@Article{MotaHincRoccSchl:2018:MoAnLO,
author = "Mota, F. A. S. and Hinckel, J. N. and Rocco, Evandro Marconi and
Schlingloff, H.",
affiliation = "{} and {} and {Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Modeling and analysis of a LOX/ethanol liquid rocket engine",
journal = "Journal of Aerospace Technology and Management",
year = "2018",
volume = "10",
number = "e3018",
keywords = "Liquid rocket engines, Ethanol, Modeling.",
abstract = "This work studies the performance and dry mass of the under
development LOX/Ethanol L75 liquid rocket engine. To this end, an
object-oriented program written in C++ was developed. The program
is intended to be versatile and easily extensible in order to
analyze different configurations of liquid rocket engines. The UML
(Unified Modeling Language) tool is used to model the architecture
of the codes. UML diagrams help to visualize the code structure
and the communication between objects, enabling a high degree of
abstraction. The cryogenics Vulcain and HM7B engines power cycles
along with the staged-combustion SSME engine perform the
verification of the codes. Finally, the influence of changes in
design parameters on the performance and dry mass of the L75
rocket engine is analyzed.",
doi = "10.5028/jatm.v10.914",
url = "http://dx.doi.org/10.5028/jatm.v10.914",
issn = "1984-9648",
language = "en",
targetfile = "mota_modeling.pdf",
urlaccessdate = "04 maio 2024"
}