Publisher
The University of Arizona.Rights
Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author.Abstract
The goal of this project is to design and manufacture 3D-printed shock isolators that mitigate high dynamic loads associated with the launch and flight of various launch vehicles. The sensitive subsystems and electrical components within launch vehicles are at risk of damage during the vehicles’ launch and flight. Shock isolators protect the components by storing shock energy and releasing it over a longer duration, reducing the shock to a non-damaging level. Our team developed three variations of shock isolator designs: a solid infill design, a hollow/ patterned infill design and casted design. We used a Formlabs Form3 Stereolithography 3D printer to print the isolators and casts. We used a proprietary resin material to create the solid and hollow infill isolators and room temperature vulcanizing compounds for the casted isolators. Each of the designs is attached to machined aluminum plates and cores. We team built a vibration and shock table with accelerometers and a concrete shaker motor to test that the isolator met the damping requirements.Type
Electronic thesistext
Degree Name
B.S.Degree Level
bachelorsDegree Program
Mechanical EngineeringHonors College