Design selection of micro-thruster system for cubesats: 1.5U-3U-6U

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριος συγγραφέας: Δούκας, Πέτρος
Μορφή: Μεταπτυχιακή εργασία
Γλώσσα:English
Έκδοση: Α.Ε.Ι. Πειραιά Τ.Τ. 2019
Θέματα:
Διαθέσιμο Online:http://okeanis.lib2.uniwa.gr/xmlui/handle/123456789/4812
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abstracttranslated The following diploma thesis deals with the design selection of micro-thruster system for 1.5U-3U-6U cubesats. In this work, they were used three different free Matlab Orbital Decay calculation programs, so as to estimate the total satellite lifetime for a space mission. In the beginning there is an extensive survey of all space missions that are smaller than 10kg. In addition, simulations are made at various heights and dimensions. Moreover there is an extensive survey of all Cubase-compatible propulsion systems and all space missions with a propulsion system. After that, all the used propellers are presented and a comparison is made in order to find the optimum in each category. In conclusion are referred the findings of the research conducted in this thesis.
advisor


author Δούκας, Πέτρος
author_facet Δούκας, Πέτρος
author_sort Δούκας, Πέτρος
collection Okeanis Institutional Repository
format Μεταπτυχιακή εργασία
id okeanis-123456789-4812
institution University of West Attica Campus II
keyword Σύστημα μικροπροώθησης
Micro-thruster system
CubeSat
Μικροδορυφόροι
language English
physical 152
publishDate 2019
publisher Α.Ε.Ι. Πειραιά Τ.Τ.
record_format dspace
spelling okeanis-123456789-48122019-03-01T12:56:26Z Design selection of micro-thruster system for cubesats: 1.5U-3U-6U Σχεδιαστική επιλογή συστήματος μικροπροώθησης σε μικροδορυφόρους: 1.5U-3U-6U Δούκας, Πέτρος Νικητάκος, Νικήτας Κούκος, Ιωάννης Μαντζούρης, Γεώργιος TPSH::Τεχνολογία Σύστημα μικροπροώθησης Micro-thruster system CubeSat Μικροδορυφόροι The following diploma thesis deals with the design selection of micro-thruster system for 1.5U-3U-6U cubesats. In this work, they were used three different free Matlab Orbital Decay calculation programs, so as to estimate the total satellite lifetime for a space mission. In the beginning there is an extensive survey of all space missions that are smaller than 10kg. In addition, simulations are made at various heights and dimensions. Moreover there is an extensive survey of all Cubase-compatible propulsion systems and all space missions with a propulsion system. After that, all the used propellers are presented and a comparison is made in order to find the optimum in each category. In conclusion are referred the findings of the research conducted in this thesis. 2019-02 Μεταπτυχιακή εργασία http://okeanis.lib2.uniwa.gr/xmlui/handle/123456789/4812 en http://creativecommons.org/licenses/by-nc-nd/3.0/gr/ Αναφορά Δημιουργού-Μη Εμπορική Χρήση-Όχι Παράγωγα Έργα 3.0 Ελλάδα Α.Ε.Ι. Πειραιά Τ.Τ. Πανεπιστήμιο Αιγαίου 152 http://okeanis.lib2.uniwa.gr/xmlui/bitstream/123456789/4812/4/ntst104.pdf.jpg
spellingShingle TPSH::Τεχνολογία
Δούκας, Πέτρος
Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title_full Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title_fullStr Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title_full_unstemmed Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title_short Design selection of micro-thruster system for cubesats: 1.5U-3U-6U
title_sort design selection of micro-thruster system for cubesats: 1.5u-3u-6u
title_translated Σχεδιαστική επιλογή συστήματος μικροπροώθησης σε μικροδορυφόρους: 1.5U-3U-6U
topic TPSH::Τεχνολογία
url http://okeanis.lib2.uniwa.gr/xmlui/handle/123456789/4812