Previous (2023-2024) Airbrakes design
Current (2024-2025) Airbrakes Design
Piston Ejection Subsystem After the apogee is reached, the descent rate must be slowed to recover the rocket safely. This is achieved by separating the rocket into two sections which are connected by a shock cord that holds the parachute. Traditionally, separation is accomplished by igniting a large black powder charge within the body tube of the rocket, pressurizing the two body tubes containing the parachute and pushing them apart. However, black powder does not burn consistently at high altitudes and this method has potential to damage the parachute. To mitigate these risks, a piston ejection system is employed. The piston ejection system consists of a piston that is activated by much smaller black powder charges that are self-contained within the piston canister. This reduces the risk of damaging the parachute and allows for reliable parachute ejection at altitudes in excess of 30,000 feet. This year, the charge canister was redesigned to allow for easier wire management, assembly, and maintenance. A burst disc was also added to the canister to ensure consistent burning of the black powder.Current (2024-2025) Piston Ejection System Design
Skills Developed by the Mechanical Team Mechanical team members are responsible for the creation of complex mechanisms from start to finish, employing and developing skills in:-
- SOLIDWORKS CAD: members gain valuable experience designing reflexive components and managing assemblies in SOLIDWORKS
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- Component analysis and design verification: using tools such as python, excel, and FEA, members rigorously ensure that mechanisms will fulfill design objectives
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- Technical drawing creation: members utilize GD&T and develop know-how in tolerancing and design for manufacturability
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- Hands-on manufacturing: using CAM and traditional manufacturing methods using mills and lathes, members create every part that we design to specified tolerances.
Finite element analysis (FEA) of airbrake drag surface (2024-2025)