A Pico-Satellite Design to Demonstrate Trajectory and Science Applications

Poster (2020)

Authors

M.S. Uludag Space Systems Egineering
S. Speretta Space Systems Egineering
A. Menicucci Space Systems Egineering
M.F. van den Bos Space Systems Egineering
C.H. Broekhuizen Space Systems Egineering
J. Haenen Student
E.K.A. Gill Space Engineering
Research Group
Space Systems Egineering
Copyright: © 2020 M.S. Uludag, S. Speretta, A. Menicucci, M.F. van den Bos, C.H. Broekhuizen, M.J.M. Bielders, J. Haenen, E.K.A. Gill
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Published Date

2020

Language

English

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Research Group

Space Systems Egineering

Abstract

This paper presents the design, integration and testing of a pico satellite, Delfi-PQ, a 3P PocketQube developed by Delft University of Technology, expected to be launched at the end of 2020. The main goal of this project is creating a miniaturized platform for future space missions with performances comparable to CubeSats, taking advantage of the miniaturization of electronic components and their integration. Education of aerospace engineering students is a second key goal of the project, where students involved in the project as part of their curricular activities.

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