@Article{MaiaGouPerVieCos:2014:DeOpCa,
author = "Maia, Fernanda Francisca and Gouv{\^e}a, Leonardo Henrique and
Pereira, Luis Gustavo Ferroni and Vieira, Ricardo and Costa,
Fernando de Souza",
affiliation = "{} and {Instituto Nacional de Pesquisas Espaciais (INPE)} and {}
and {Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Development and optimization of a catalytic thruster for hydrogen
peroxide decomposition",
journal = "Journal of Aerospace Technology and Management",
year = "2014",
volume = "6",
number = "1",
pages = "61--67",
month = "Jan.-Mar.",
keywords = "satellite propulsion, hydrogen peroxide, mixed oxide catalyst,
catalytic bed optimization.",
abstract = "Hydrogen peroxide is a non toxic, low cost, green onopropellant
with a significant potential for applications in satellite
microthrusters. It presents a density-specific impulse similar to
hydrazine. A new bulk mixed oxide catalyst for decomposition of
hydrogen peroxide has been developed and tested in a 2 N thruster
with modular parts, allowing the use of catalytic beds with
different diameters and lengths. A method of experiment design
with a star configuration was implemented to optimize the
catalytic bed geometry, in order to yield complete peroxide
decomposition, reduce thruster size and volume and provide maximum
thrust.",
doi = "10.5028/jatm.v6i1.286",
url = "http://dx.doi.org/10.5028/jatm.v6i1.286",
issn = "1984-9648",
label = "scopus 2014-05 MaiaGouPerVieCos:2014:DeOpCa",
language = "en",
targetfile = "286-1663-1-PB.pdf",
urlaccessdate = "27 abr. 2024"
}