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...
Guardado en:
| Autores principales: | , , , |
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| Formato: | Objeto de conferencia |
| Lenguaje: | Inglés |
| Publicado: |
2014
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| Materias: | |
| Acceso en línea: | http://sedici.unlp.edu.ar/handle/10915/55532 http://www.aero.ing.unlp.edu.ar/caia/Actas-CAIA3/44.pdf |
| Aporte de: |
| id |
I19-R120-10915-55532 |
|---|---|
| record_format |
dspace |
| 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 http://www.aero.ing.unlp.edu.ar/caia/Actas-CAIA3/44.pdf |
| work_keys_str_mv |
AT murciaj flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom AT gomezs flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom AT ceronmunozh flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom AT portillag flightpathanalysisinsoundingrocketlibertadoriwithcomputationalsimulationonthreedegreesoffreedom |
| bdutipo_str |
Repositorios |
| _version_ |
1764820476997140482 |