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

Alejandro Urrego

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 flight –simulated 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 exposed as follows.


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References


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DOI: http://dx.doi.org/10.18180/tecciencia.2019.27.8

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