A mechanical clamp design for NASA
Clamp designed in Catia V5R21
The vector forces acting on the interface plate.
The DWG files drafted in 3d modelling, CAE
The mechanism in exploded view with Balloons.
The sensor plates
The section view AA across the mechanism.
The ISS handrail and clamp.
The mass calculation for Part manufacturing/material aquisition.
The Static stress analysis after FEM meshing/parabolic in Catia V5R21 with one end fixed and axial load of 4 N
Regards
creative space engineering
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