@Article{HennemannAndrCost:2014:ExInMo,
author = "Hennemann, Luciano and Andrade, Jos{\'e} Carlos de and Costa,
Fernando de Souza",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)}",
title = "Experimental Investigation of a Monopropellant Thruster Using
Nitrous Oxide",
journal = "Journal of Aerospace Technology and Management",
year = "2014",
volume = "6",
number = "4",
pages = "363--372",
month = "Oct.-Dec.",
note = "{Setores de Atividade: Pesquisa e desenvolvimento
cient{\'{\i}}fico.}",
keywords = "satellite propulsion, nitrous oxide, rhodium oxide catalyst,
propulsive efficiency.",
abstract = "Nitrous oxide is a monopropellant with potential for use in
propulsion systems for orbit correction, positioning and attitude
control of satellites. This paper presents experimental results
with a 2N thruster prototype employing nitrous oxide gas
decomposed by a rhodium oxide catalyst supported on alumina.
Initially, the thruster design, the test bench and test
procedures are described. Then the main experimental results,
including thrust curves, mass flow rates, pressures and
temperatures along the thruster are presented for pulsed
operation. At the end specific impulses, characteristic velocities
and thruster efficiencies are determined, thus indicating a
catalytic decomposition efficiency of about 88%.",
doi = "10.5028/jatm.v6i4.382",
url = "http://dx.doi.org/10.5028/jatm.v6i4.382",
issn = "1984-9648",
label = "lattes: 6600426630222951 3 HennemannAndrCost:2014:ExInMo",
language = "en",
targetfile = "382-2207-2-PB.pdf",
url = "http://www.jatm.com.br/ojs/index.php/jatm/article/view/382/pdf_36",
urlaccessdate = "23 abr. 2024"
}