Caterina Busso
Preliminary Mission Analysis and Sub-System Design for the 16U4SBSP CubeSat Mission.
Rel. Manuela Battipede. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2024
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Abstract
The mission concept “16U4SBSP”, funded by the European Space Agency through the Sysnova campaign “Innovative Missions Concepts enabled by Swarms of Cube- Sats”, aims to demonstrate the feasibility of a swarm of 16U CubeSats for a scaled demonstration of Space-Based Solar Power (SBSP). This demonstration mission can provide wireless electric energy in kW-scale to space-to-ground or space-to-space applications. The main objective of the mission is to validate the SBSP concept and some of the involved technologies, in view of full-scale missions which could serve users in remote areas with low power requirements (<MW) or/and emergency operations in the blackout zones affected by natural or manmade hazards.
The focus of this master thesis is the study of the mission’s formation flying orbital dynamics for the case of Heliotropic orbits and the study of the thermal analysis and thermal design of the CubeSats
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