@InProceedings{TikamiSant:2015:RePiLa,
author = "Tikami, Auro and Santos, Walter Abrah{\~a}o dos",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Re-engineering a Picosatellite for a Langmuir Probe Payload",
booktitle = "Anais...",
year = "2015",
organization = "Workshop em Engenharia e Tecnologia Espaciais, 6. (WETE)",
keywords = "picosatellite, sonda Langmuir, system re-engineering, space
systems.",
abstract = "Miniaturized satellites are being used for a myriad of missions
previously not conceived for such class of devices due to their
attractive cost-benefits. This work has a case study focused in a
picosatellite, named Tancredo 1, which has been re-engineered from
a standard TubeSat platform. It is expected to be launched by
early 2016 from the Kibo (\き\ぼ\う, Japanese
for hope) Japan Aerospace Exploration Agency (JAXA) module of the
International Space Station (ISS) from which it will be released.
Using the ISS infrastructure has imposed a new set of safety
requirements to this project and new system re-engineering tasks.
As part of INPE´s Aeronomy research demands, the picosatellite
mission has also added a second payload, a Langmuir probe which
also imposed extra requirements and changes that this work
describes briefly.",
conference-location = "S{\~a}o Jos{\'e} dos Campos, SP",
conference-year = "18-19 ago",
label = "lattes: 4522542236886713 1 TikamiSant:2015:RePiLa",
language = "en",
targetfile = "15_[ARTIGO] auro.pdf",
url = "http://urlib.net/8JMKD3MGP3W/3KN2MNS",
urlaccessdate = "17 maio 2024"
}