SSM-System

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My name is Tomás Mucciacciaro, I am a mechanical engineering student at the Faculty of Exact Sciences, Engineering and Surveying (FCEIA) of the National University of Rosario, Santa Fe, Argentina (UNR): FCEIA-UNRThis is a practical work for the subject M-25 Synthesis of Mechanisms and Machines, directed by Professor Marcelo Valderrey , and corresponds to the edition of this subject taken during the first quarter of 2024.It is a work based on the results of NASA CHALLENGE for which I formally give credit to all its participants and explain, in the attached file, the use that I have given to their ideas and models during a practice of "Convergent Divergent Creative Postprocessing" that is part of the design method that I study in this subject. After the analysis and classification of these solutions, a new proposal emerges. The designers have done great work, each with their own particular approach, from my point of view I would take the solution to the simplest of all possible ones, where no additional complexity is required, either for the use of the module itself, or for the construction of it. A simple static system is proposed, which, giving up a little load capacity in volume, meeting (and exceeding) the proposed objectives, significantly increases the simplicity of construction of the module and its reliability, since, by not depending on movement devices . , nor devices that stop it in the takeoff phase, greatly increase reliability.Based on the proposed solution NASA Challenge: Lunar Gateway Cargo Packing and Storing by Stéphane Gazel , this idea arises. The big problem I see with this solution is, as the author shows, the number of movements that must be made to access certain loads.At this moment is where the idea of ​​better this charge extraction arises, and combine it with the Nasa challenge : Cube in tube by Mhmd Bsl for the charge extraction mechanism between rings. In this way the design is a static system, separated into rings to which the load is fixed, spaced a sufficient distance for the crew member to enter and remove the load.The system for securing loads to the ring is the one proposed in Lunar Gateway Hambar L.M. CTPE 410 by Mustafa ÇOBANOĞLU