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Structures and Mechanisms
Constructed of 6061-T6 Aluminum and 6Al-4V Titanium Four-legged square-shaped body Able to withstand 5.5g’s upon launch Able to withstand impact force upon landing 797,600 N
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Structures and Mechanisms
Finite Element Analysis of Vertical Member of Lander Body Using Von Mises Max Stress Criterion FS=8.8
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Structures and Mechanisms
Finite Element Analysis of Vertical Member of Lander Body Using Von Mises Max Stress Criterion FS=1.3
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Structures and Mechanisms
Finite Element Analysis of Landing Leg Strut Using Von Mises Max Stress Criterion FS=3.1
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