@MastersThesis{Contaifer:2009:DeBaTe,
author = "Contaifer, Ricardo Amaral",
title = "Desenvolvimento de uma bancada de testes de propulsores
h{\'{\i}}bridos de baixo empuxo",
school = "Instituto Nacional de Pesquisas Espaciais (INPE)",
year = "2009",
address = "S{\~a}o Jos{\'e} dos Campos",
month = "2009-06-29",
keywords = "foguete h{\'{\i}}brido, parafina, {\'o}xido nitroso, bancada de
teste, hybrid rocket, paraffin, nitrous oxide, test stand.",
abstract = "A busca por propulsores de baixo custo, boa confiabilidade, baixo
impacto ambiental e n{\'{\i}}vel de seguran{\c{c}}a elevado
aumentam o interesse pelo desenvolvimento dos propulsores
h{\'{\i}}bridos. Este trabalho descreve o projeto, a
constru{\c{c}}{\~a}o e a operacionaliza{\c{c}}{\~a}o de uma
bancada de testes de propulsores h{\'{\i}}bridos com empuxo
at{\'e} 500 N. Um propulsor h{\'{\i}}brido de 400 N usando
parafina s{\'o}lida como combust{\'{\i}}vel e {\'o}xido
nitroso l{\'{\i}}quido como oxidante foi projetado,
constru{\'{\i}}do e testado na bancada. O propulsor conta com
sistema de inje{\c{c}}{\~a}o centr{\'{\i}}fugo, ignitor
eletrot{\'e}rmico catal{\'{\i}}tico e tubeira refrigerada. A
bancada permite testes com press{\~o}es at{\'e} 150 bar no
tanque de oxidante e vaz{\~o}es at{\'e} 600 kg/h do oxidante e
disp{\~o}e de sistema de aquisi{\c{c}}{\~a}o e controle com 32
canais. ABSTRACT: The quest for thrusters of low cost, good
reliability, low environmental impact and high safety levels
increased the interest for development of hybrid thrusters. This
work describes the design, construction and operationalization of
a stand for testing hybrid thrusters with thrusts up to 500 N. A
400 N hybrid thruster using solid paraffin as fuel and nitrous
oxide as oxidizer was designed, built and tested in the stand. The
thruster includes a pressure swirl injector, an electro thermal
catalytic ignitor and nozzles with and without water cooling. The
stand allows tests with oxidizer tank pressures up to 150 bar,
oxidant mass flow rates up to 600 kg/h controlled by Coriolis flow
meter and controller and includes a data acquisition and control
system with 32 channels.",
committee = "Costa, Fernando de Souza (presidente/orientador) and Netto,
Dam{\'e}trio Bastos and Veras, Carlos Alberto Gurgel",
copyholder = "SID/SCD",
englishtitle = "Design of a test stand of hybrid rockets",
language = "pt",
pages = "191",
ibi = "8JMKD3MGP8W/35RA9D5",
url = "http://urlib.net/ibi/8JMKD3MGP8W/35RA9D5",
targetfile = "publicacao.pdf",
urlaccessdate = "2024, Apr. 29"
}