Design and Construction of a Flight Data Acquisition System Adapted to an Experimental Rocket Model

Authors

  • J. Alejandro Urrego P. Programa de Ingeniería Aeronáutica. Facultad de Ingeniería. Universidad de San Buenaventura, sede Bogotá-Colombia
  • Luisa Mónico Programa de Ingeniería Aeronáutica. Facultad de Ingeniería. Universidad de San Buenaventura, sede Bogotá-Colombia.
  • Harold Acosta Programa de Ingeniería Aeronáutica. Facultad de Ingeniería. Universidad de San Buenaventura, sede Bogotá-Colombia.
  • Germán Reyes
  • Luis Hernández Programa de Ingeniería Aeronáutica. Facultad de Ingeniería. Universidad de San Buenaventura, sede Bogotá-Colombia

Keywords:

Data acquisition, Experimental rocketry, Solid fuel, Raspberry Pi, Micro-electro-mechanical systems

Abstract

This document describes the different stages of development need to design, build and characterize a flight data acquisition system for the experimental rocket USB - Rocket I. To do so, some simulated flight conditions collected from a computer program, and the manufacturing and assembly process of an integrated electronic circuit are presented. As a result, the flight data collected in a horizontal ground displacement and commercial flight test are presented with this device.

Published

2021-04-01

How to Cite

Urrego P., J. A. ., Mónico, L., Acosta, H. ., Reyes, G. ., & Hernández, L. (2021). Design and Construction of a Flight Data Acquisition System Adapted to an Experimental Rocket Model. Tecciencia, 14(27), 73–83. Retrieved from https://tecciencia.ecci.edu.co/index.php/TECCIENCIA/article/view/112