Giuseppe Partipilo
Tailoring of development and verification activities for an in-orbit technology demonstration CubeSat.
Rel. Sabrina Corpino, Fabrizio Stesina. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2024
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Abstract
Over the past two decades, CubeSats have emerged as a viable and competitive alternative for accessing space, compared to classical, monolithic satellite designs. Initially conceived as relatively affordable way for universities to access space, mainly for academic and research objectives, CubeSats have shown growing potential as versatile platforms for various purposes, such as Earth observation and in-orbit technology demonstration. Their relatively low cost and fast time of delivery have attracted the interest of not only universities, but also governmental agencies and commercial companies. Over time, it became clear that it was neither efficient nor effective to treat CubeSats as "scaled down" version of larger satellites: instead, tailored methodologies for satellite design and verification were developed, often preferring agile and less restrictive solutions over traditional document-heavy approaches.
The main goal of this thesis is to formally document some of the tailored methodologies and processes developed for CubeSat design, development and verification, and to investigate how to implement them in the feasibility analysis of a real-life case study: the in-orbit technology demonstration CubeSat project DELETE, which, at the time of this thesis' publication, is being developed at Thales Alenia Space Italia, one of the major players in the European space sector
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