Diseño de la estructura de un cohete de tres etapas para transportar una carga útil de 200 kg a una órbita baja de la Tierra
This article presents the conceptual design of the structure of a three-stage rocket capable of carrying 200 kg to low Earth orbits, developed in the project of grade of two students of aeronautical engineering from the Fundación Universitaria Los Libertadores. The design starts from the decision of...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Escuela de Posgrados de la Fuerza Aérea Colombiana
2019-09-01
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| Series: | Ciencia y Poder Aéreo |
| Subjects: | |
| Online Access: | https://doi.org/10.18667/cienciaypoderaereo.627 |