Victor's Team has received the following awards and nominations. Way to go!
The existing solution used by NASA is ZipNuts, which requires applying torque to turn the outer nut to lock/unlock it. In a space environment where both time and tooling are incredibly restricted, it is desirable to make this process simpler and not require torque to fasten a connection. Thus we designed what I call the Compliant Axial Lockable Fastening System (CALFS). It replaces a traditional threaded fastener in terms of functionality and operates completely axially.
We are mechanical engineers by trade, so this project immediately appealed to us. We started off with lots of conceptual sketches of mechanisms, created CAD, verified the operation of the compliant mechanisms via FEM, 3D printed and tested prototypes, and reiterated until the prototype worked and was presentable.
The most useful resources that were referenced were the comments from the NASA SMEs in the Space Apps Chat, as well as the provided examples of in-space assembly technology like ZipNuts.
Slides (including a super short video) here:
https://docs.google.com/presentation/d/11L9YzDeaDXoOzmwoPQC_9UE3_zKn6uB34Hlwnc6of_Y/edit
https://www.nasa.gov/missions/science/zipnuts.html
Another resource I read and found helpful was the book “Handbook of Compliant Mechanisms” by L.L. Howell et al.