Design, analysis and optimization of a micro-satellite for the study of lower thermosphere and re-entry conditions

The scope of this thesis is to design, built and test a Double-Unit nanosatellite, with the view of launching and operate it in the lower thermosphere. The key innovative approach is the design optimization for an actual space mission, creating a hybrid design for the structural subsystem. The new d...

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Bibliographic Details
Main Author: Αμπατζόγλου, Ανδρέας
Other Authors: Κωστόπουλος, Βασίλης
Format: Thesis
Language:English
Published: 2017
Subjects:
Online Access:http://hdl.handle.net/10889/10553