Estudio del funcionamiento y factibilidad del rediseño del motor SUA II
The purpose of this project is to present a design for a LOX tank and the feed system for the liquid propellant phase of the AINKA VI rocket. This design is expected to correct some of the rockets current problems, such as improving the feed system reliability under harsh and expected flight conditi...
- Autores:
-
Toro Márquez, Santiago
- Tipo de recurso:
- Trabajo de grado de pregrado
- Fecha de publicación:
- 2025
- Institución:
- Universidad de los Andes
- Repositorio:
- Séneca: repositorio Uniandes
- Idioma:
- spa
- OAI Identifier:
- oai:repositorio.uniandes.edu.co:1992/75384
- Acceso en línea:
- https://hdl.handle.net/1992/75384
- Palabra clave:
- Cohetes
Experimentación
Sistemas de alimentación
Alimentación por presurización
Oxígeno Líquido
Combustión Líquida
Ingeniería
- Rights
- openAccess
- License
- Attribution-NonCommercial-NoDerivatives 4.0 International
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Séneca: repositorio Uniandes |
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|
dc.title.none.fl_str_mv |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
title |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
spellingShingle |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II Cohetes Experimentación Sistemas de alimentación Alimentación por presurización Oxígeno Líquido Combustión Líquida Ingeniería |
title_short |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
title_full |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
title_fullStr |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
title_full_unstemmed |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
title_sort |
Estudio del funcionamiento y factibilidad del rediseño del motor SUA II |
dc.creator.fl_str_mv |
Toro Márquez, Santiago |
dc.contributor.advisor.none.fl_str_mv |
Rojas Mora, Fabio Arturo |
dc.contributor.author.none.fl_str_mv |
Toro Márquez, Santiago |
dc.subject.keyword.spa.fl_str_mv |
Cohetes Experimentación Sistemas de alimentación Alimentación por presurización Oxígeno Líquido Combustión Líquida |
topic |
Cohetes Experimentación Sistemas de alimentación Alimentación por presurización Oxígeno Líquido Combustión Líquida Ingeniería |
dc.subject.themes.spa.fl_str_mv |
Ingeniería |
description |
The purpose of this project is to present a design for a LOX tank and the feed system for the liquid propellant phase of the AINKA VI rocket. This design is expected to correct some of the rockets current problems, such as improving the feed system reliability under harsh and expected flight conditions, such as vibrations, oscillation, and rotations. A first prototype was proposed alongside an experiment to evaluate the concept, which is expected to be worked on in the future to optimize the design and finally integrate it inside of the rocket and assess it in a real launch. |
publishDate |
2025 |
dc.date.accessioned.none.fl_str_mv |
2025-01-13T21:52:21Z |
dc.date.available.none.fl_str_mv |
2025-01-13T21:52:21Z |
dc.date.issued.none.fl_str_mv |
2025-01-10 |
dc.type.none.fl_str_mv |
Trabajo de grado - Pregrado |
dc.type.driver.none.fl_str_mv |
info:eu-repo/semantics/bachelorThesis |
dc.type.version.none.fl_str_mv |
info:eu-repo/semantics/acceptedVersion |
dc.type.coar.none.fl_str_mv |
http://purl.org/coar/resource_type/c_7a1f |
dc.type.content.none.fl_str_mv |
Text |
dc.type.redcol.none.fl_str_mv |
http://purl.org/redcol/resource_type/TP |
format |
http://purl.org/coar/resource_type/c_7a1f |
status_str |
acceptedVersion |
dc.identifier.uri.none.fl_str_mv |
https://hdl.handle.net/1992/75384 |
dc.identifier.instname.none.fl_str_mv |
instname:Universidad de los Andes |
dc.identifier.reponame.none.fl_str_mv |
reponame:Repositorio Institucional Séneca |
dc.identifier.repourl.none.fl_str_mv |
repourl:https://repositorio.uniandes.edu.co/ |
url |
https://hdl.handle.net/1992/75384 |
identifier_str_mv |
instname:Universidad de los Andes reponame:Repositorio Institucional Séneca repourl:https://repositorio.uniandes.edu.co/ |
dc.language.iso.none.fl_str_mv |
spa |
language |
spa |
dc.rights.en.fl_str_mv |
Attribution-NonCommercial-NoDerivatives 4.0 International |
dc.rights.uri.none.fl_str_mv |
http://creativecommons.org/licenses/by-nc-nd/4.0/ |
dc.rights.accessrights.none.fl_str_mv |
info:eu-repo/semantics/openAccess |
dc.rights.coar.none.fl_str_mv |
http://purl.org/coar/access_right/c_abf2 |
rights_invalid_str_mv |
Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/ http://purl.org/coar/access_right/c_abf2 |
eu_rights_str_mv |
openAccess |
dc.format.extent.none.fl_str_mv |
54 páginas |
dc.format.mimetype.none.fl_str_mv |
application/pdf |
dc.publisher.none.fl_str_mv |
Universidad de los Andes |
dc.publisher.program.none.fl_str_mv |
Ingeniería Mecánica |
dc.publisher.faculty.none.fl_str_mv |
Facultad de Ingeniería |
dc.publisher.department.none.fl_str_mv |
Departamento de Ingeniería Mecánica |
publisher.none.fl_str_mv |
Universidad de los Andes |
institution |
Universidad de los Andes |
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Al consultar y hacer uso de este recurso, está aceptando las condiciones de uso establecidas por los autoresAttribution-NonCommercial-NoDerivatives 4.0 Internationalhttp://creativecommons.org/licenses/by-nc-nd/4.0/info:eu-repo/semantics/openAccesshttp://purl.org/coar/access_right/c_abf2Rojas Mora, Fabio Arturovirtual::22033-1Toro Márquez, Santiago2025-01-13T21:52:21Z2025-01-13T21:52:21Z2025-01-10https://hdl.handle.net/1992/75384instname:Universidad de los Andesreponame:Repositorio Institucional Sénecarepourl:https://repositorio.uniandes.edu.co/The purpose of this project is to present a design for a LOX tank and the feed system for the liquid propellant phase of the AINKA VI rocket. This design is expected to correct some of the rockets current problems, such as improving the feed system reliability under harsh and expected flight conditions, such as vibrations, oscillation, and rotations. A first prototype was proposed alongside an experiment to evaluate the concept, which is expected to be worked on in the future to optimize the design and finally integrate it inside of the rocket and assess it in a real launch.Pregrado54 páginasapplication/pdfspaUniversidad de los AndesIngeniería MecánicaFacultad de IngenieríaDepartamento de Ingeniería MecánicaEstudio del funcionamiento y factibilidad del rediseño del motor SUA IITrabajo de grado - Pregradoinfo:eu-repo/semantics/bachelorThesisinfo:eu-repo/semantics/acceptedVersionhttp://purl.org/coar/resource_type/c_7a1fTexthttp://purl.org/redcol/resource_type/TPCohetesExperimentaciónSistemas de alimentaciónAlimentación por presurizaciónOxígeno LíquidoCombustión 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