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A Pico-Satellite Design to Demonstrate Trajectory and Science Applications

Authors :
Uludag, M.S. (author)
Speretta, S. (author)
Menicucci, A. (author)
van den Bos, M.F. (author)
Broekhuizen, C.H. (author)
Bielders, M.J.M. (author)
Haenen, J. (author)
Gill, E.K.A. (author)
Uludag, M.S. (author)
Speretta, S. (author)
Menicucci, A. (author)
van den Bos, M.F. (author)
Broekhuizen, C.H. (author)
Bielders, M.J.M. (author)
Haenen, J. (author)
Gill, E.K.A. (author)
Publication Year :
2020

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.<br />Clean Room<br />Space Systems Egineering<br />Space Engineering

Details

Database :
OAIster
Notes :
English
Publication Type :
Electronic Resource
Accession number :
edsoai.on1245662157
Document Type :
Electronic Resource