Project Overview
The objective of our team was to design, build, and fly a high-powered rocket to compete in NASA’s annual Student Launch Challenge. The first goal was to create a new rocket design that emphasized recovery reliability and had the ability to be fully disassembled for inspection and repairing purposes. The second goal was to create better means of testing the rocket’s subsystems on the ground. The final product was Uncertainty, this year’s full-scale rocket, which flew 4800ft and had a successful recovery. The rocket has a 2-stage recovery system that allows the rocket to break apart into three sections and deploy 2 parachutes to slow its descent to the ground. By removing an inch off the rocket’s diameter compared to last year’s design, from 6in to 5in, the total weight of the rocket decreased from 55lbs to 45.4lbs; a 17.5% reduction. Another significant change was the use of screws to attach structural components to the body tube rather than the use of epoxy. The use of screws made the rocket fully deconstructable and allowed stronger materials, like aluminum, to be used for structural components. Advances in parachute packing also resulted in 100% parachute deployment reliability during launch tests. The creation of systems such as a custom pop-test rig and an avionics bay vibration chamber allowed the team to confidently test the rocket’s subsystems. The rocket is also responsible for safely carrying the payload team’s project during flight. Our team designed attachment points in the nosecone and worked with the payload team to protect sensitive electronics onboard. This team is part of AIAA, a nationally recognized aerospace association. Our team within AIAA, the Zenith Program, allows undergraduate students to get first-hand experience in rocket design and fabrication; and is the backbone of this project.
Team Members

Dylan Hampton
Systems Integration Engineer
Mechanical Engineering Department

Adrian Arocha
Vehicle Engineer
Mechanical Engineering Department

Wyatt Abrams
Recovery Engineer
Mechanical Engineering Department

Carter Thomas
Separations Engineer
Electrical Engineering Department

Adin Weatherby
Avionics Engineer
Electrical Engineering Department

Logan Shvartsman
Materials Engineer
Mechanical Engineering Department
Project Leadership

Sponsor
Shayne McConomy, Ph.D.
Professor
Mechanical Engineering Department

Advisor
Chiang Shih, Ph.D.
Professor
Mechanical Engineering Department
Project Timeline
Project Proposal
September 2024
In the beginning stages of the project the general goals for the year are presented along with team members and their respective roles.
Preliminary Design Review
September 2024
With a team in place, initial designs are created for both a full scale and subscale rocket.
Prototype Subscale Presentation
December 2024
After a semester of designing a building, a working ready to fly subscale rocket is presented and any design changes are made.
Critical Design Review
January 2025
A successful subscale flight is presented along with essential selections including the motor, target apogee, and other important metrics.
Full Scale Build and Demonstration Flight
March 2025
As students progress through the spring semester the full scale rocket is fabricated, utilizing resources including FSU's innovation hub and the College of Engineering's machine shop.
Flight Readiness Review
March 2025
After the successful build and launch of the full scale, all final design choices are presented to NASA, including frequenceies used on launch day.
NASA Flight
April 2025
The day the entire project leads up to- Launch Day! The team is launching from home this year due to a scheduling conflict with launch day falling on graduation day, but all data will be sent to NASA following this launch.
Post- Launch Assessment Review
April 2025
Once the final launch is complete, a final report including important aspects of the launch is created for NASA and the team is scored in competetion.