Recovery is a critical, but often overlooked, rocket system. Project Prometheus had one of the most successful recovery systems in MIT Rocket Team’s recent history. Its two members were Ariella Blackman (Class of 2027) and Elizabeth Jackson (Class of 2027), with assistance and guidance from our Team Lead, Ezra Eyre (Class of 2026), and Project Phoenix and Medusa Recovery Engineer, Jenna Blair (Class of 2026). Overall, the subteam accomplished a lot and was able to test new experimental deployment systems, design and manufacture their own parachutes, and test their system during Prometheus Test Launch.
Timeline was as follows:
October: First Design Cycle
November: PDR, Second Design Cycle
December: CDR
January-March: Manufacturing and Testing
April: Test Launch
May: Failure and Success Analysis
The Design was based off of the requirements from Spaceport that required a drogue parachute if hitting above 2,000 ft of altitude. Each of our two stages (Booster and Sustainer) had two parachutes (Drogue and Main), both mains were purchased from Rocketman Parachutes and the drogues were designed and manufactured by the team. The new deployment mechanism that we used was a black powder ejection technique that was for three of our parachutes. Due to altitude, the fourth parachute had a piston assembly instead.
We had a 75% success rate (three out of four total parachutes) with deployment during Test Launch. While we were not satisfied with this result, this is the most successful Recovery System in the last 4 years. After Test Launch we completed a failure analysis and discussed important changes that we want to make going forward.
In summary, Project Prometheus’s Recovery System went through an entire engineering cycle with successes and important lessons about recovery learned. Below are details on components and guides to how we accomplished what we did, and what we would like to do better.
Test Launch and Failure Analysis
Our guiding equation for sizing parachutes:
We used our calculator (linked here) to help us determine how we would size our rocket based on the original values we were given for terminal velocity and the coefficient of drag. We made this calculator so that we would be able to change the sizes of the parachute as both the terminal velocity and the coefficient of drag were things that could change over the course of the semester.
For our two main parachutes we decided to buy them from Rocketman Chutes, (linked here). For our drogue parachutes we decided that we wanted to design and manufacture them ourselves. To do this we chose a simple octogonal design with a small eye hole (based off of previous drogue parachutes on Phoenix). We finalized these designs before the end of the design cycle in December.
Manufacturing of the drogue parachutes took place during IAP 2024. Overall, this was one of the more time consuming and careful manufacturing jobs that recovery completed for Project Prometheus and included some failures in addition to successes.
*Note on Nylon Webbing in Successes and Failures section
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