Bachelor Thesis from the year 2014 in the subject Engineering - Aerospace Technology, grade: 10/10, Universidad Europea de Madrid, language: English, abstract: The whole Cubesat functionality depends on the integrity of its subsystems. For that reason, it is very important that the structure subsystem is built to be robust and reliable to ensure the protection of all other subsystems integrated within. The goal is to develop a high performance Cubesat structure with the use of new materials, like composite materials. The use of composite materials for primary structure increases the strength and reduces the weight of existing Cubesat structures increasing at the same time the payload capacity. Interplanetary missions require more robust and reliable structures so a Cubesat manufactured with composite materials could be the solution for those exploratory missions. One of the keys of a composite structure is the design in order to reduce manufacturing cost and stress concentration, especially on interference with other components. The results of study on alternative structures designs for Cubesat, shows that one solid wall composite Cubesat design can stand up to 25g loads with a temperature range of -55°C (-67° F) to 90°C (194° F). Additionally, the vibration simulation results show a minimum vibration mode of 157.6 Hz. All of that was achieved with a weight of 183 grams.
Produktkennzeichnungen
ISBN-10
3656854785
ISBN-13
9783656854784
eBay Product ID (ePID)
211226170
Produkt Hauptmerkmale
Sprache
Englisch
Anzahl der Seiten
108 Seiten
Verlag
Grin Publishing
Publikationsname
Alternative Structure Design For Cubesat
Autor
Gustavo Cotta Vallina
Format
Taschenbuch
Erscheinungsjahr
2015
Zusätzliche Produkteigenschaften
Hörbuch
No
Item Length
21cm
Item Height
7mm
Ausgabe
Ausgabe Nr. 1 des Jahres 15
Item Width
14cm
Item Weight
169g
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