Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom

This paper presents obtained results from computer simulations in order to analyze the flight path of the sounding rocket Libertador I, developed in 2012 at the Fundación Universitaria Los Libertadores. The main aspects that affect the motion of a rocket are propulsion and aerodynamics effects. Nu...

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Autores principales: Murcia, J., Gomez, S., Cerón Muñoz, H., Portilla, G.
Formato: Objeto de conferencia
Lenguaje:Inglés
Publicado: 2014
Materias:
Ingeniería Aeronáutica
Simulación
trayectoria de vuelo
rocket motor
solid propellant
sounding rocket
Acceso en línea:http://sedici.unlp.edu.ar/handle/10915/55532
Aporte de:
SEDICI (UNLP) de Universidad Nacional de La Plata
id I19-R120-10915-55532
record_format dspace
spelling I19-R120-10915-555322023-09-21T17:36:10Z http://sedici.unlp.edu.ar/handle/10915/55532 Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom Murcia, J. Gomez, S. Cerón Muñoz, H. Portilla, G. 2014-11 2014 2016-10-04T11:47:55Z en Ingeniería Aeronáutica Simulación trayectoria de vuelo rocket motor solid propellant sounding rocket This paper presents obtained results from computer simulations in order to analyze the flight path of the sounding rocket Libertador I, developed in 2012 at the Fundación Universitaria Los Libertadores. The main aspects that affect the motion of a rocket are propulsion and aerodynamics effects. Numerical algorithms were implemented to value the thrust provided by the rocket motor as well as aerodynamic loads. Then, the differential equations of the motion are solved using the Runge-Kutta method, RK9. Trajectory and other numerical results are calculated from a code developed in FORTRAN. Finally, graphs of the flight path, curves of the vehicle velocity as function of time are presented. Also, the algorithm permits to determine the maximum altitude and possible impact sites. Facultad de Ingeniería Objeto de conferencia Objeto de conferencia http://creativecommons.org/licenses/by/4.0/ Creative Commons Attribution 4.0 International (CC BY 4.0) application/pdf
institution Universidad Nacional de La Plata
institution_str I-19
repository_str R-120
collection SEDICI (UNLP)
language Inglés
topic Ingeniería Aeronáutica
Simulación
trayectoria de vuelo
rocket motor
solid propellant
sounding rocket
spellingShingle Ingeniería Aeronáutica
Simulación
trayectoria de vuelo
rocket motor
solid propellant
sounding rocket
Murcia, J.
Gomez, S.
Cerón Muñoz, H.
Portilla, G.
Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
topic_facet Ingeniería Aeronáutica
Simulación
trayectoria de vuelo
rocket motor
solid propellant
sounding rocket
description This paper presents obtained results from computer simulations in order to analyze the flight path of the sounding rocket Libertador I, developed in 2012 at the Fundación Universitaria Los Libertadores. The main aspects that affect the motion of a rocket are propulsion and aerodynamics effects. Numerical algorithms were implemented to value the thrust provided by the rocket motor as well as aerodynamic loads. Then, the differential equations of the motion are solved using the Runge-Kutta method, RK9. Trajectory and other numerical results are calculated from a code developed in FORTRAN. Finally, graphs of the flight path, curves of the vehicle velocity as function of time are presented. Also, the algorithm permits to determine the maximum altitude and possible impact sites.
format Objeto de conferencia
Objeto de conferencia
author Murcia, J.
Gomez, S.
Cerón Muñoz, H.
Portilla, G.
author_facet Murcia, J.
Gomez, S.
Cerón Muñoz, H.
Portilla, G.
author_sort Murcia, J.
title Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
title_short Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
title_full Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
title_fullStr Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
title_full_unstemmed Flight path analysis in sounding rocket “Libertador I” with computational simulation on three degrees of freedom
title_sort flight path analysis in sounding rocket “libertador i” with computational simulation on three degrees of freedom
publishDate 2014
url http://sedici.unlp.edu.ar/handle/10915/55532
work_keys_str_mv AT murciaj flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom
AT gomezs flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom
AT ceronmunozh flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom
AT portillag flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom
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