@Article{MarchiMurcPradSoló:2017:InMiCi,
author = "Marchi, Luis Ot{\'a}vio and Murcia, J. O. and Prado, Antonio
Fernando Bertachini de Almeida and Sol{\'o}rzano, C R H",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {} and
{Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Universidade Federal do ABC}",
title = "Injection of a microsatellite in circular orbits using a
three-stage launch vehicle",
journal = "Journal of Physics: Conference Series",
year = "2017",
volume = "911",
pages = "012012",
keywords = "Astrodin{\^a}mica.",
abstract = "The injection of a satellite into orbit is usually done by a
multi-stage launch vehicle. Nowadays, the space market
demonstrates a strong tendency towards the use of smaller
satellites, because the miniaturization of the systems improve the
cost/benefit of a mission. A study to evaluate the capacity of the
Brazilian Microsatellite Launch Vehicle (VLM) to inject payloads
into Low Earth Orbits is presented in this paper. All launches are
selected to be made to the east side of the Alc{\^a}ntara Launch
Center (CLA). The dynamical model to calculate the trajectory
consists of the three degrees of freedom (3DOF) associated with
the translational movement of the rocket. Several simulations are
performed according to a set of restrictions imposed to the
flight. The altitude reached in the separation of the second
stage, the altitude and velocity of injection, the flight path
angle at the moment of the activation of the third stage and the
duration of the ballistic flight are presented as a function of
the payload carried.",
doi = "10.1088/1742-6596/911/1/012012",
url = "http://dx.doi.org/10.1088/1742-6596/911/1/012012",
issn = "1742-6588",
label = "lattes: 7340081273816424 3 MarchiMurcPradSol{\'o}:2017:InMiCi",
language = "pt",
targetfile = "marchi_injection.pdf",
urlaccessdate = "27 abr. 2024"
}