The structural analysis and optimization of the SM machine model stabilizes the structure of the fuselage and provides the best high dynamic rigidity when the machine moves at high speed.
SM-1613; SM-2113; SM-2613;
SM-1618; SM-2118; SM-2618; SM-3118;
SM-2118Y; SM-2618Y; SM-3118Y;
SM-2622; SM-3122; SM-4122; SM-5122; SM-6122;
SM-2622Y; SM-3122Y; SM-4122Y, SM-5122Y; SM-6122Y;
SM-2622E; SA-3122E; SM4122E; SM-5122E; SM-6122E
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