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
| Summary: | 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. |
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