Awards & Nominations
milky way has received the following awards and nominations. Way to go!

milky way has received the following awards and nominations. Way to go!
We created a mechanical release mechanism, designed to separate two components of a spacecraft. The design consists of a cylindrical screw component housing a compressed spring (attached to one of the two components), and a rotating cap (attached to the second component). By rotating the cap, the cap is “unlocked” from the cylindrical component, allowing the compressed spring to release its potential energy and push the two components apart. Our design is superior to pyrotechnics, as our smoother release mechanism allows for greater reusability and prevents damage to nearby components. Additionally, our simple design means the separation process will be quick and reliable.
The project in itself is a replacement to the currently used pyrotechnic bolts by NASA in their satellites and as a form of separation. This replacement we developed is a spring-loaded bolt that transitions from the use of pyrotechnics to something that could function much smoother. By having a low impact reusable bolt such as this one we can lower manufacturing costs, not only for the bolt but for all surrounding parts. Our solution creates no space debris. It can withstand preloads of 1800N with a factor of safety of 2 makings, in addition only containing 3 parts in the system (outer casing, cap, and spring) this makes our solution very reliable. All of this is achieved while abiding by the 44mm long and 10mm diameter constraint as well as being fully reusable. The development/testing of this project was primarily done through the use of CAD where the design could be visualized and certain restrictions and variables set on it such as the material and other contributing factors. The main hope for the project and the design is to be able to remove the concerns and situations that NASA may encounter through their use of pyrotechnics such as potential hazards, it is an explosion after all, along with the factor of space debris by installing something that is fairly simple to construct, easy to function and is most importantly reusable.
Throughout the design process, we were inspired by the docking systems used on previous spacecraft. Both the Apollo, and Space Shuttle spacecraft were capable of docking and decoupling without the use of pyrotechnic bolts. The process had to happen multiple times so components could not be damaged.
Thus we often looked to diagrams of past spacecraft (two of which are below) to help inspire our design. It is because of these designs that we looked to incorporate a spring mechanism and an “unlocking” mechanism into our design.
https://www.hq.nasa.gov/alsj/CSM11_Docking_Subsystem_pp87-92.pdf
https://www.nasa.gov/pdf/593865main_AP_ST_Phys_ShuttleODS.pdf
https://ntrs.nasa.gov/api/citations/19840017027/downloads/19840017027.pdf
Additionally many of the materials that we tested and used where based off the materials that NASA had listed which are used for manufacturing parts for use in space or during launch.
This hackathon was one of the most instructional and funnest experiences that I personally had and I'm sure my team would agree. With basically no prior experience for most of the team we learnt:
We are all freshman aerospace engineering students so this challenge was not only interesting to us but also a great opportunity to learn all these relevant skills as opposed to a more coding oriented challenge which have less to do to our major and interests.
The approach we took was one of flexibility and constant iteration. It was rare to go 30 minutes without a question or criticism which would make major changes to our designs.
Big thanks to you guys for setting this up, my teammates for being down to do this, Jose Mojica the ESDC manager and Prakhar Agarwal for making accommodations and opening the center for us to be able to print over the weekend.
SolidWorks 2021 (for 3D models and structural simulation and analysis)
Spring Simulator
https://www.thespringstore.com/free-spring-calculator-software.html
Resources for Materials
https://www.thomasnet.com/articles/hardware/aerospace-fastener-types/
https://www.aerospacemanufacturinganddesign.com/article/aluminum-alloys-for-aerospace/
Docking Examples
https://www.hq.nasa.gov/alsj/CSM11_Docking_Subsystem_pp87-92.pdf
https://www.nasa.gov/pdf/593865main_AP_ST_Phys_ShuttleODS.pdf
https://ntrs.nasa.gov/api/citations/19840017027/downloads/19840017027.pdf
#hardware
This project has been submitted for consideration during the Judging process.
Letting things go in space, or separating spacecraft parts, is often a violent, high-shock event. Your challenge is to design a mechanical separation device that can cut a parachute reefing line, a bolt for an adapter ring, or a cable, or release two parts from each other smoothly in space without pyrotechnics.
